SlideShare uma empresa Scribd logo
1 de 52
Fluid Mechanics and Thermodynamics<br />Weekly Assessed Tutorial Sheets,<br />Student Sheets: WATS 10.<br />The WATS approach to assessment was developed as part of an LTSN Engineering Mini-Project, funded at the University of Hertfordshire which aimed to develop a set of 'student unique' tutorial sheets to actively encourage and improve student participation within a first year first ‘fluid mechanics and thermodynamics’ module. Please see the accompanying Mini-Project Report “Improving student success and retention through greater participation and tackling student-unique tutorial sheets” for more information.<br />The WATS cover core Fluid Mechanics and Thermodynamics topics at first year undergraduate level. 11 tutorial sheets and their worked solutions are provided here for you to utilise in your teaching. The variables within each question can be altered so that each student answers the same question but will need to produce a unique solution.<br />FURTHER INFORMATION<br />Please see http://tinyurl.com/2wf2lfh to access the WATS Random Factor Generating Wizard. <br />There are also explanatory videos on how to use the Wizard and how to implement WATS available at http://www.youtube.com/user/MBRBLU#p/u/7/0wgC4wy1cV0 and http://www.youtube.com/user/MBRBLU#p/u/6/MGpueiPHpqk.<br />For more information on WATS, its use and impact on students please contact Mark Russell, School of Aerospace, Automotive and Design Engineering at University of Hertfordshire.<br /> <br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number1EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.33 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 325 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.74  m.<br />Q2) 18.30 kg/s of air enters a turbine at 980 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 174 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.33  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number2EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 415 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.53  m.<br />Q2) 15.40 kg/s of air enters a turbine at 640 °C with a velocity of 75 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.59  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number3EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.45 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 220 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.38  m.<br />Q2) 11.00 kg/s of air enters a turbine at 570 °C with a velocity of 54 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 138 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.21  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number4EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 270 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.64  m.<br />Q2) 9.10 kg/s of air enters a turbine at 640 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 154 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.72  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number5EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.28 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 400 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.40  m.<br />Q2) 8.40 kg/s of air enters a turbine at 650 °C with a velocity of 65 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 170 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.53  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number6EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.23 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 405 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.63  m.<br />Q2) 6.80 kg/s of air enters a turbine at 780 °C with a velocity of 84 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 134 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.17  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number7EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 280 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.65  m.<br />Q2) 11.80 kg/s of air enters a turbine at 1030 °C with a velocity of 52 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 110 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.77  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number8EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 450 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42  m.<br />Q2) 14.10 kg/s of air enters a turbine at 500 °C with a velocity of 70 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 114 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.17  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number9EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 315 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.63  m.<br />Q2) 5.80 kg/s of air enters a turbine at 1130 °C with a velocity of 98 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 126 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.86  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number10EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.50 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 230 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42  m.<br />Q2) 7.40 kg/s of air enters a turbine at 700 °C with a velocity of 69 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 146 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.87  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number11EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.42 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 435 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.34  m.<br />Q2) 13.10 kg/s of air enters a turbine at 1160 °C with a velocity of 67 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 116 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.08  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number12EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 240 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.41  m.<br />Q2) 5.60 kg/s of air enters a turbine at 800 °C with a velocity of 99 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 148 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.66  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number13EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.47 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 255 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.71  m.<br />Q2) 17.90 kg/s of air enters a turbine at 610 °C with a velocity of 54 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 128 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.73  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number14EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.21 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 395 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.58  m.<br />Q2) 10.20 kg/s of air enters a turbine at 860 °C with a velocity of 75 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 174 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.20  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number15EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.25 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 355 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.67  m.<br />Q2) 12.80 kg/s of air enters a turbine at 1150 °C with a velocity of 84 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 160 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.58  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number16EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.50 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 335 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.63  m.<br />Q2) 9.30 kg/s of air enters a turbine at 1080 °C with a velocity of 75 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 164 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.20  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number17EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.46 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 385 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.36  m.<br />Q2) 19.80 kg/s of air enters a turbine at 640 °C with a velocity of 90 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 110 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.00  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number18EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.47 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 295 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.54  m.<br />Q2) 15.20 kg/s of air enters a turbine at 690 °C with a velocity of 64 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 112 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 5.00  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number19EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.43 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 215 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42  m.<br />Q2) 9.80 kg/s of air enters a turbine at 540 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 112 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.94  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number20EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.31 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 330 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.46  m.<br />Q2) 16.30 kg/s of air enters a turbine at 680 °C with a velocity of 84 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 120 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.86  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number21EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.50 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 430 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.47  m.<br />Q2) 6.30 kg/s of air enters a turbine at 940 °C with a velocity of 79 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 168 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.54  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number22EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.28 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 290 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.69  m.<br />Q2) 6.60 kg/s of air enters a turbine at 950 °C with a velocity of 52 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 124 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.99  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number23EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 340 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.64  m.<br />Q2) 12.00 kg/s of air enters a turbine at 670 °C with a velocity of 98 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 166 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.58  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number24EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.21 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 395 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.36  m.<br />Q2) 5.60 kg/s of air enters a turbine at 1200 °C with a velocity of 74 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 124 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.35  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number25EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.47 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 340 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.31  m.<br />Q2) 14.90 kg/s of air enters a turbine at 1070 °C with a velocity of 88 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 178 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.67  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number26EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.25 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 365 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.65  m.<br />Q2) 5.30 kg/s of air enters a turbine at 620 °C with a velocity of 72 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.23  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number27EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.27 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 320 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.41  m.<br />Q2) 13.10 kg/s of air enters a turbine at 840 °C with a velocity of 82 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 166 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.14  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number28EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.20 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 365 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.68  m.<br />Q2) 12.00 kg/s of air enters a turbine at 510 °C with a velocity of 74 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 126 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.50  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number29EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 385 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.35  m.<br />Q2) 12.80 kg/s of air enters a turbine at 850 °C with a velocity of 96 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 176 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.73  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number30EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.41 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 245 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.52  m.<br />Q2) 16.60 kg/s of air enters a turbine at 770 °C with a velocity of 59 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 132 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.67  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number31EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.27 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 395 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.62  m.<br />Q2) 15.60 kg/s of air enters a turbine at 750 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 140 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.01  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number32EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.35 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 375 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.33  m.<br />Q2) 13.30 kg/s of air enters a turbine at 830 °C with a velocity of 77 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 160 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.71  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number33EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.21 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 300 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.46  m.<br />Q2) 9.60 kg/s of air enters a turbine at 650 °C with a velocity of 78 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 118 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.53  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number34EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.30 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 260 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.61  m.<br />Q2) 7.50 kg/s of air enters a turbine at 670 °C with a velocity of 68 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 134 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.59  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number35EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 320 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.69  m.<br />Q2) 8.30 kg/s of air enters a turbine at 860 °C with a velocity of 74 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 122 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.79  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number36EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.33 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 235 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.60  m.<br />Q2) 12.60 kg/s of air enters a turbine at 670 °C with a velocity of 58 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 170 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.53  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number37EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 395 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.67  m.<br />Q2) 19.90 kg/s of air enters a turbine at 1100 °C with a velocity of 73 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 122 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.86  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number38EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.35 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 230 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.75  m.<br />Q2) 19.60 kg/s of air enters a turbine at 950 °C with a velocity of 53 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 156 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.13  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number39EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.34 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 245 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.33  m.<br />Q2) 18.50 kg/s of air enters a turbine at 620 °C with a velocity of 66 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 114 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.84  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number40EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.46 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 310 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.38  m.<br />Q2) 16.40 kg/s of air enters a turbine at 800 °C with a velocity of 56 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 114 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.10  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number41EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 445 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42  m.<br />Q2) 10.80 kg/s of air enters a turbine at 580 °C with a velocity of 60 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 154 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.00  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number42EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.23 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 340 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.44  m.<br />Q2) 10.90 kg/s of air enters a turbine at 1180 °C with a velocity of 90 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 174 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.82  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number43EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.44 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 345 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.79  m.<br />Q2) 14.80 kg/s of air enters a turbine at 970 °C with a velocity of 53 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 124 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.74  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number44EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.40 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 395 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.39  m.<br />Q2) 11.60 kg/s of air enters a turbine at 1050 °C with a velocity of 91 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.66  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number45EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 300 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.33  m.<br />Q2) 14.10 kg/s of air enters a turbine at 530 °C with a velocity of 87 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 134 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.22  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number46EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.20 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 275 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.70  m.<br />Q2) 13.80 kg/s of air enters a turbine at 880 °C with a velocity of 53 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 166 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.02  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number47EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 435 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.60  m.<br />Q2) 19.40 kg/s of air enters a turbine at 1100 °C with a velocity of 99 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 130 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.81  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number48EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.44 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 325 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.48  m.<br />Q2) 18.00 kg/s of air enters a turbine at 720 °C with a velocity of 95 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 118 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.09  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number49EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 270 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.43  m.<br />Q2) 14.40 kg/s of air enters a turbine at 850 °C with a velocity of 94 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 110 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.26  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number50EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.35 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 310 ° C.  Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.75  m.<br />Q2) 7.80 kg/s of air enters a turbine at 580 °C with a velocity of 88 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.45  MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Credits<br />This resource was created by the University of Hertfordshire and released as an open educational resource through the Open Engineering Resources project of the HE Academy Engineering Subject Centre. The Open Engineering Resources project was funded by HEFCE and part of the JISC/HE Academy UKOER programme.<br />© University of Hertfordshire 2009<br />This work is licensed under a Creative Commons Attribution 2.0 License. <br />The name of the University of Hertfordshire, UH and the UH logo are the name and registered marks of the University of Hertfordshire. To the fullest extent permitted by law the University of Hertfordshire reserves all its rights in its name and marks which may not be used except with its written permission.<br />The JISC logo is licensed under the terms of the Creative Commons Attribution-Non-Commercial-No Derivative Works 2.0 UK: England & Wales Licence.  All reproductions must comply with the terms of that licence.<br />The HEA logo is owned by the Higher Education Academy Limited may be freely distributed and copied for educational purposes only, provided that appropriate acknowledgement is given to the Higher Education Academy as the copyright holder and original publisher.<br />
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics
WATS 10 (1-50) Fluid Mechanics and Thermodynamics

Mais conteúdo relacionado

Mais procurados

Energy performance assessment of boilers
Energy performance assessment of boilersEnergy performance assessment of boilers
Energy performance assessment of boilers
Utsav Jain
 
Estimating The Available Amount Of Waste Heat
Estimating The Available Amount Of Waste HeatEstimating The Available Amount Of Waste Heat
Estimating The Available Amount Of Waste Heat
harlandmachacon
 
Combustion & Flue Gas Analysis
Combustion & Flue Gas AnalysisCombustion & Flue Gas Analysis
Combustion & Flue Gas Analysis
Amit Makwana
 
ME 490_HaydenYoungs_FinalReport.FinalCopy
ME 490_HaydenYoungs_FinalReport.FinalCopyME 490_HaydenYoungs_FinalReport.FinalCopy
ME 490_HaydenYoungs_FinalReport.FinalCopy
Hayden Youngs
 
Fuels and combustion (2014)
Fuels and combustion (2014)Fuels and combustion (2014)
Fuels and combustion (2014)
Yuri Melliza
 

Mais procurados (20)

Energy performance assessment of boilers
Energy performance assessment of boilersEnergy performance assessment of boilers
Energy performance assessment of boilers
 
Estimating The Available Amount Of Waste Heat
Estimating The Available Amount Of Waste HeatEstimating The Available Amount Of Waste Heat
Estimating The Available Amount Of Waste Heat
 
Combustion & Flue Gas Analysis
Combustion & Flue Gas AnalysisCombustion & Flue Gas Analysis
Combustion & Flue Gas Analysis
 
Lab 1 the dryness fraction of the steam(mech)
Lab 1   the dryness fraction of the steam(mech)Lab 1   the dryness fraction of the steam(mech)
Lab 1 the dryness fraction of the steam(mech)
 
Design With Solid works Software and Planning Calculation Analysis of Fire Tu...
Design With Solid works Software and Planning Calculation Analysis of Fire Tu...Design With Solid works Software and Planning Calculation Analysis of Fire Tu...
Design With Solid works Software and Planning Calculation Analysis of Fire Tu...
 
LECTURE Notes on compressor
LECTURE Notes on compressorLECTURE Notes on compressor
LECTURE Notes on compressor
 
2007 AFRC-JFRC Flare Tip Analysis Using CFD
2007 AFRC-JFRC Flare Tip Analysis Using CFD2007 AFRC-JFRC Flare Tip Analysis Using CFD
2007 AFRC-JFRC Flare Tip Analysis Using CFD
 
Lecture 16b Chemical Reactions and Combustion
Lecture 16b Chemical Reactions and CombustionLecture 16b Chemical Reactions and Combustion
Lecture 16b Chemical Reactions and Combustion
 
ME 490_HaydenYoungs_FinalReport.FinalCopy
ME 490_HaydenYoungs_FinalReport.FinalCopyME 490_HaydenYoungs_FinalReport.FinalCopy
ME 490_HaydenYoungs_FinalReport.FinalCopy
 
Boy's gas calorimeter
Boy's gas calorimeterBoy's gas calorimeter
Boy's gas calorimeter
 
Final lab report for thermos 2(mech)
Final lab report for thermos 2(mech)Final lab report for thermos 2(mech)
Final lab report for thermos 2(mech)
 
Thermodynamics chapter 3
Thermodynamics chapter 3Thermodynamics chapter 3
Thermodynamics chapter 3
 
Combustion and fules
Combustion and fulesCombustion and fules
Combustion and fules
 
Energy Efficiency of Industrial Utilities
Energy Efficiency of Industrial UtilitiesEnergy Efficiency of Industrial Utilities
Energy Efficiency of Industrial Utilities
 
Combined separating and throttling calorimeter
Combined separating and throttling  calorimeterCombined separating and throttling  calorimeter
Combined separating and throttling calorimeter
 
Assessment of boiler performance
Assessment of boiler performanceAssessment of boiler performance
Assessment of boiler performance
 
Boiler design-calculation 3
Boiler design-calculation 3Boiler design-calculation 3
Boiler design-calculation 3
 
Board exam on druyers
Board exam on druyersBoard exam on druyers
Board exam on druyers
 
Heat 4
Heat 4Heat 4
Heat 4
 
Fuels and combustion (2014)
Fuels and combustion (2014)Fuels and combustion (2014)
Fuels and combustion (2014)
 

Destaque

Atuação do enfermeiro na prevenção das úlceras por pressão na hospitalização
Atuação do enfermeiro na prevenção das úlceras por pressão na hospitalizaçãoAtuação do enfermeiro na prevenção das úlceras por pressão na hospitalização
Atuação do enfermeiro na prevenção das úlceras por pressão na hospitalização
Rafaela Correia
 
Tesf2
Tesf2Tesf2
Tesf2
CHRIS
 
Recuperação Judicial
Recuperação JudicialRecuperação Judicial
Recuperação Judicial
Henrique Arake
 
S O C I A L N E T W O R K I N G P R O J E C T
S O C I A L  N E T W O R K I N G  P R O J E C TS O C I A L  N E T W O R K I N G  P R O J E C T
S O C I A L N E T W O R K I N G P R O J E C T
CKillinger
 
บทที่ 2 วิวัฒนาการมัลติมีเดีย
บทที่ 2 วิวัฒนาการมัลติมีเดียบทที่ 2 วิวัฒนาการมัลติมีเดีย
บทที่ 2 วิวัฒนาการมัลติมีเดีย
somdetpittayakom school
 
Power Point Conte Laura I Companyia
Power Point Conte Laura I CompanyiaPower Point Conte Laura I Companyia
Power Point Conte Laura I Companyia
guest12122153
 
SETTEC Training Plan 2013
SETTEC Training Plan 2013SETTEC Training Plan 2013
SETTEC Training Plan 2013
SETTEC
 
Deportes durante la guerra fría 2
Deportes durante la guerra fría 2Deportes durante la guerra fría 2
Deportes durante la guerra fría 2
Bernardo Berríos
 
Presentation1
Presentation1Presentation1
Presentation1
jhommes5
 

Destaque (20)

Professional Development: Distance Learning Opportunities (Museums, Science C...
Professional Development: Distance Learning Opportunities (Museums, Science C...Professional Development: Distance Learning Opportunities (Museums, Science C...
Professional Development: Distance Learning Opportunities (Museums, Science C...
 
Atuação do enfermeiro na prevenção das úlceras por pressão na hospitalização
Atuação do enfermeiro na prevenção das úlceras por pressão na hospitalizaçãoAtuação do enfermeiro na prevenção das úlceras por pressão na hospitalização
Atuação do enfermeiro na prevenção das úlceras por pressão na hospitalização
 
Acquisition & analysis of neurologic data
Acquisition & analysis of neurologic dataAcquisition & analysis of neurologic data
Acquisition & analysis of neurologic data
 
Tesf2
Tesf2Tesf2
Tesf2
 
Recuperação Judicial
Recuperação JudicialRecuperação Judicial
Recuperação Judicial
 
Pavimentos
PavimentosPavimentos
Pavimentos
 
Portfolio Pp
Portfolio PpPortfolio Pp
Portfolio Pp
 
Salespeopledothedarndestthings Productcamp2010 100327111717 Phpapp02
Salespeopledothedarndestthings Productcamp2010 100327111717 Phpapp02Salespeopledothedarndestthings Productcamp2010 100327111717 Phpapp02
Salespeopledothedarndestthings Productcamp2010 100327111717 Phpapp02
 
S O C I A L N E T W O R K I N G P R O J E C T
S O C I A L  N E T W O R K I N G  P R O J E C TS O C I A L  N E T W O R K I N G  P R O J E C T
S O C I A L N E T W O R K I N G P R O J E C T
 
ABS
ABSABS
ABS
 
emka TECHNOLOGIES - solutions for primates
emka TECHNOLOGIES - solutions for primatesemka TECHNOLOGIES - solutions for primates
emka TECHNOLOGIES - solutions for primates
 
Tesf
TesfTesf
Tesf
 
Rau Dang Sau He
Rau Dang Sau HeRau Dang Sau He
Rau Dang Sau He
 
บทที่ 2 วิวัฒนาการมัลติมีเดีย
บทที่ 2 วิวัฒนาการมัลติมีเดียบทที่ 2 วิวัฒนาการมัลติมีเดีย
บทที่ 2 วิวัฒนาการมัลติมีเดีย
 
Power Point Conte Laura I Companyia
Power Point Conte Laura I CompanyiaPower Point Conte Laura I Companyia
Power Point Conte Laura I Companyia
 
Waseet Profile -March 20010
Waseet Profile -March 20010Waseet Profile -March 20010
Waseet Profile -March 20010
 
SETTEC Training Plan 2013
SETTEC Training Plan 2013SETTEC Training Plan 2013
SETTEC Training Plan 2013
 
Culture Of Contact
Culture Of ContactCulture Of Contact
Culture Of Contact
 
Deportes durante la guerra fría 2
Deportes durante la guerra fría 2Deportes durante la guerra fría 2
Deportes durante la guerra fría 2
 
Presentation1
Presentation1Presentation1
Presentation1
 

Semelhante a WATS 10 (1-50) Fluid Mechanics and Thermodynamics

Mech 0036 exam 12 13 with answers (revision)
Mech 0036 exam 12 13  with answers (revision)Mech 0036 exam 12 13  with answers (revision)
Mech 0036 exam 12 13 with answers (revision)
Mostafa Tamish
 

Semelhante a WATS 10 (1-50) Fluid Mechanics and Thermodynamics (20)

ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2011
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2011ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2011
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2011
 
Me2202 engineering thermodynamics uq - april may 2011
Me2202 engineering thermodynamics   uq -  april may 2011Me2202 engineering thermodynamics   uq -  april may 2011
Me2202 engineering thermodynamics uq - april may 2011
 
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014.
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014.ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014.
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014.
 
Me2202 engineering thermodynamics uq - april may 2011
Me2202 engineering thermodynamics   uq - april may 2011Me2202 engineering thermodynamics   uq - april may 2011
Me2202 engineering thermodynamics uq - april may 2011
 
Me2202 engineering thermodynamics uq - april may 2010
Me2202 engineering thermodynamics   uq - april may 2010Me2202 engineering thermodynamics   uq - april may 2010
Me2202 engineering thermodynamics uq - april may 2010
 
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2014
 
Me2202 engineering thermodynamics uq - may june 2014
Me2202 engineering thermodynamics   uq - may june 2014Me2202 engineering thermodynamics   uq - may june 2014
Me2202 engineering thermodynamics uq - may june 2014
 
Me6301 engineering thermodynamics uq - may june 2016
Me6301 engineering thermodynamics   uq - may june 2016Me6301 engineering thermodynamics   uq - may june 2016
Me6301 engineering thermodynamics uq - may june 2016
 
X10694 (me8391)
X10694 (me8391)X10694 (me8391)
X10694 (me8391)
 
Engineering thermodynamics
Engineering thermodynamicsEngineering thermodynamics
Engineering thermodynamics
 
Me2202 engineering thermodynamics uq - nov dec 2015
Me2202 engineering thermodynamics   uq - nov dec 2015Me2202 engineering thermodynamics   uq - nov dec 2015
Me2202 engineering thermodynamics uq - nov dec 2015
 
Me2202 engineering thermodynamics uq - nov dec 2011
Me2202 engineering thermodynamics   uq - nov dec 2011Me2202 engineering thermodynamics   uq - nov dec 2011
Me2202 engineering thermodynamics uq - nov dec 2011
 
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2007
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2007ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2007
ME6301 ENGINEERING THERMODYNAMICS ANNA UNIVERSITY QUESTION PAPER may june 2007
 
Me6301 engineering thermodynamics uq - nov dec 2018
Me6301 engineering thermodynamics   uq - nov dec 2018Me6301 engineering thermodynamics   uq - nov dec 2018
Me6301 engineering thermodynamics uq - nov dec 2018
 
Me2202 engineering thermodynamics uq - nov dec 2014
Me2202 engineering thermodynamics   uq - nov dec 2014Me2202 engineering thermodynamics   uq - nov dec 2014
Me2202 engineering thermodynamics uq - nov dec 2014
 
Mech 0036 exam 12 13 with answers (revision)
Mech 0036 exam 12 13  with answers (revision)Mech 0036 exam 12 13  with answers (revision)
Mech 0036 exam 12 13 with answers (revision)
 
WATS 7 (1-50) Fluid Mechanics and Thermodynamics
WATS 7 (1-50) Fluid Mechanics and ThermodynamicsWATS 7 (1-50) Fluid Mechanics and Thermodynamics
WATS 7 (1-50) Fluid Mechanics and Thermodynamics
 
Me2202 engineering thermodynamics uq - nov dec 2010
Me2202 engineering thermodynamics   uq - nov dec 2010Me2202 engineering thermodynamics   uq - nov dec 2010
Me2202 engineering thermodynamics uq - nov dec 2010
 
Me1201 engineering thermodynamics uq - may june 2007
Me1201 engineering thermodynamics   uq -  may june 2007Me1201 engineering thermodynamics   uq -  may june 2007
Me1201 engineering thermodynamics uq - may june 2007
 
Me6301 engineering thermodynamics uq - nov dec 2015
Me6301 engineering thermodynamics   uq - nov dec 2015Me6301 engineering thermodynamics   uq - nov dec 2015
Me6301 engineering thermodynamics uq - nov dec 2015
 

Mais de Mark Russell

Iblc10 making an existing assessment more efficient
Iblc10   making an existing assessment more efficientIblc10   making an existing assessment more efficient
Iblc10 making an existing assessment more efficient
Mark Russell
 

Mais de Mark Russell (11)

Iblc10 making an existing assessment more efficient
Iblc10   making an existing assessment more efficientIblc10   making an existing assessment more efficient
Iblc10 making an existing assessment more efficient
 
Two-Dimension Steady-State Conduction
Two-Dimension Steady-State ConductionTwo-Dimension Steady-State Conduction
Two-Dimension Steady-State Conduction
 
WATS 9 (1-50) Fluid Mechanics and Thermodynamics
WATS 9 (1-50) Fluid Mechanics and ThermodynamicsWATS 9 (1-50) Fluid Mechanics and Thermodynamics
WATS 9 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 8 (1-50) Fluid Mechanics and Thermodynamics
WATS 8 (1-50) Fluid Mechanics and ThermodynamicsWATS 8 (1-50) Fluid Mechanics and Thermodynamics
WATS 8 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 6 (1-50) Fluid Mechanics and Thermodynamics
WATS 6 (1-50) Fluid Mechanics and ThermodynamicsWATS 6 (1-50) Fluid Mechanics and Thermodynamics
WATS 6 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 5 (1-50) Fluid Mechanics and Thermodynamics
WATS 5 (1-50) Fluid Mechanics and ThermodynamicsWATS 5 (1-50) Fluid Mechanics and Thermodynamics
WATS 5 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 1 (1-50) Fluid Mechanics and Thermodynamics
WATS 1 (1-50) Fluid Mechanics and ThermodynamicsWATS 1 (1-50) Fluid Mechanics and Thermodynamics
WATS 1 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 4 (1-50) Fluid Mechanics and Thermodynamics
WATS 4 (1-50) Fluid Mechanics and ThermodynamicsWATS 4 (1-50) Fluid Mechanics and Thermodynamics
WATS 4 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 3 (1-50) Fluid Mechanics and Thermodynamics
WATS 3 (1-50) Fluid Mechanics and ThermodynamicsWATS 3 (1-50) Fluid Mechanics and Thermodynamics
WATS 3 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 2 (1-50) Fluid Mechanics and Thermodynamics
WATS 2 (1-50) Fluid Mechanics and ThermodynamicsWATS 2 (1-50) Fluid Mechanics and Thermodynamics
WATS 2 (1-50) Fluid Mechanics and Thermodynamics
 
WATS 11 (1-50) Fluid Mechanics and Thermodynamics
WATS 11 (1-50)  Fluid Mechanics and ThermodynamicsWATS 11 (1-50)  Fluid Mechanics and Thermodynamics
WATS 11 (1-50) Fluid Mechanics and Thermodynamics
 

Último

Vishram Singh - Textbook of Anatomy Upper Limb and Thorax.. Volume 1 (1).pdf
Vishram Singh - Textbook of Anatomy  Upper Limb and Thorax.. Volume 1 (1).pdfVishram Singh - Textbook of Anatomy  Upper Limb and Thorax.. Volume 1 (1).pdf
Vishram Singh - Textbook of Anatomy Upper Limb and Thorax.. Volume 1 (1).pdf
ssuserdda66b
 
Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...
Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...
Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...
ZurliaSoop
 
Salient Features of India constitution especially power and functions
Salient Features of India constitution especially power and functionsSalient Features of India constitution especially power and functions
Salient Features of India constitution especially power and functions
KarakKing
 
1029-Danh muc Sach Giao Khoa khoi 6.pdf
1029-Danh muc Sach Giao Khoa khoi  6.pdf1029-Danh muc Sach Giao Khoa khoi  6.pdf
1029-Danh muc Sach Giao Khoa khoi 6.pdf
QucHHunhnh
 

Último (20)

2024-NATIONAL-LEARNING-CAMP-AND-OTHER.pptx
2024-NATIONAL-LEARNING-CAMP-AND-OTHER.pptx2024-NATIONAL-LEARNING-CAMP-AND-OTHER.pptx
2024-NATIONAL-LEARNING-CAMP-AND-OTHER.pptx
 
Vishram Singh - Textbook of Anatomy Upper Limb and Thorax.. Volume 1 (1).pdf
Vishram Singh - Textbook of Anatomy  Upper Limb and Thorax.. Volume 1 (1).pdfVishram Singh - Textbook of Anatomy  Upper Limb and Thorax.. Volume 1 (1).pdf
Vishram Singh - Textbook of Anatomy Upper Limb and Thorax.. Volume 1 (1).pdf
 
Application orientated numerical on hev.ppt
Application orientated numerical on hev.pptApplication orientated numerical on hev.ppt
Application orientated numerical on hev.ppt
 
HMCS Max Bernays Pre-Deployment Brief (May 2024).pptx
HMCS Max Bernays Pre-Deployment Brief (May 2024).pptxHMCS Max Bernays Pre-Deployment Brief (May 2024).pptx
HMCS Max Bernays Pre-Deployment Brief (May 2024).pptx
 
Unit-V; Pricing (Pharma Marketing Management).pptx
Unit-V; Pricing (Pharma Marketing Management).pptxUnit-V; Pricing (Pharma Marketing Management).pptx
Unit-V; Pricing (Pharma Marketing Management).pptx
 
Holdier Curriculum Vitae (April 2024).pdf
Holdier Curriculum Vitae (April 2024).pdfHoldier Curriculum Vitae (April 2024).pdf
Holdier Curriculum Vitae (April 2024).pdf
 
SOC 101 Demonstration of Learning Presentation
SOC 101 Demonstration of Learning PresentationSOC 101 Demonstration of Learning Presentation
SOC 101 Demonstration of Learning Presentation
 
FSB Advising Checklist - Orientation 2024
FSB Advising Checklist - Orientation 2024FSB Advising Checklist - Orientation 2024
FSB Advising Checklist - Orientation 2024
 
Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...
Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...
Jual Obat Aborsi Hongkong ( Asli No.1 ) 085657271886 Obat Penggugur Kandungan...
 
Towards a code of practice for AI in AT.pptx
Towards a code of practice for AI in AT.pptxTowards a code of practice for AI in AT.pptx
Towards a code of practice for AI in AT.pptx
 
ICT Role in 21st Century Education & its Challenges.pptx
ICT Role in 21st Century Education & its Challenges.pptxICT Role in 21st Century Education & its Challenges.pptx
ICT Role in 21st Century Education & its Challenges.pptx
 
Salient Features of India constitution especially power and functions
Salient Features of India constitution especially power and functionsSalient Features of India constitution especially power and functions
Salient Features of India constitution especially power and functions
 
Sociology 101 Demonstration of Learning Exhibit
Sociology 101 Demonstration of Learning ExhibitSociology 101 Demonstration of Learning Exhibit
Sociology 101 Demonstration of Learning Exhibit
 
1029-Danh muc Sach Giao Khoa khoi 6.pdf
1029-Danh muc Sach Giao Khoa khoi  6.pdf1029-Danh muc Sach Giao Khoa khoi  6.pdf
1029-Danh muc Sach Giao Khoa khoi 6.pdf
 
Python Notes for mca i year students osmania university.docx
Python Notes for mca i year students osmania university.docxPython Notes for mca i year students osmania university.docx
Python Notes for mca i year students osmania university.docx
 
Single or Multiple melodic lines structure
Single or Multiple melodic lines structureSingle or Multiple melodic lines structure
Single or Multiple melodic lines structure
 
Spatium Project Simulation student brief
Spatium Project Simulation student briefSpatium Project Simulation student brief
Spatium Project Simulation student brief
 
ComPTIA Overview | Comptia Security+ Book SY0-701
ComPTIA Overview | Comptia Security+ Book SY0-701ComPTIA Overview | Comptia Security+ Book SY0-701
ComPTIA Overview | Comptia Security+ Book SY0-701
 
Google Gemini An AI Revolution in Education.pptx
Google Gemini An AI Revolution in Education.pptxGoogle Gemini An AI Revolution in Education.pptx
Google Gemini An AI Revolution in Education.pptx
 
How to Manage Global Discount in Odoo 17 POS
How to Manage Global Discount in Odoo 17 POSHow to Manage Global Discount in Odoo 17 POS
How to Manage Global Discount in Odoo 17 POS
 

WATS 10 (1-50) Fluid Mechanics and Thermodynamics

  • 1. Fluid Mechanics and Thermodynamics<br />Weekly Assessed Tutorial Sheets,<br />Student Sheets: WATS 10.<br />The WATS approach to assessment was developed as part of an LTSN Engineering Mini-Project, funded at the University of Hertfordshire which aimed to develop a set of 'student unique' tutorial sheets to actively encourage and improve student participation within a first year first ‘fluid mechanics and thermodynamics’ module. Please see the accompanying Mini-Project Report “Improving student success and retention through greater participation and tackling student-unique tutorial sheets” for more information.<br />The WATS cover core Fluid Mechanics and Thermodynamics topics at first year undergraduate level. 11 tutorial sheets and their worked solutions are provided here for you to utilise in your teaching. The variables within each question can be altered so that each student answers the same question but will need to produce a unique solution.<br />FURTHER INFORMATION<br />Please see http://tinyurl.com/2wf2lfh to access the WATS Random Factor Generating Wizard. <br />There are also explanatory videos on how to use the Wizard and how to implement WATS available at http://www.youtube.com/user/MBRBLU#p/u/7/0wgC4wy1cV0 and http://www.youtube.com/user/MBRBLU#p/u/6/MGpueiPHpqk.<br />For more information on WATS, its use and impact on students please contact Mark Russell, School of Aerospace, Automotive and Design Engineering at University of Hertfordshire.<br /> <br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number1EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.33 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 325 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.74 m.<br />Q2) 18.30 kg/s of air enters a turbine at 980 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 174 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.33 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number2EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 415 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.53 m.<br />Q2) 15.40 kg/s of air enters a turbine at 640 °C with a velocity of 75 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.59 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number3EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.45 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 220 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.38 m.<br />Q2) 11.00 kg/s of air enters a turbine at 570 °C with a velocity of 54 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 138 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.21 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number4EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 270 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.64 m.<br />Q2) 9.10 kg/s of air enters a turbine at 640 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 154 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.72 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number5EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.28 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 400 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.40 m.<br />Q2) 8.40 kg/s of air enters a turbine at 650 °C with a velocity of 65 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 170 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.53 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number6EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.23 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 405 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.63 m.<br />Q2) 6.80 kg/s of air enters a turbine at 780 °C with a velocity of 84 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 134 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.17 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number7EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 280 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.65 m.<br />Q2) 11.80 kg/s of air enters a turbine at 1030 °C with a velocity of 52 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 110 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.77 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number8EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 450 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42 m.<br />Q2) 14.10 kg/s of air enters a turbine at 500 °C with a velocity of 70 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 114 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.17 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number9EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 315 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.63 m.<br />Q2) 5.80 kg/s of air enters a turbine at 1130 °C with a velocity of 98 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 126 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.86 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number10EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.50 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 230 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42 m.<br />Q2) 7.40 kg/s of air enters a turbine at 700 °C with a velocity of 69 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 146 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.87 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number11EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.42 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 435 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.34 m.<br />Q2) 13.10 kg/s of air enters a turbine at 1160 °C with a velocity of 67 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 116 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.08 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number12EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 240 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.41 m.<br />Q2) 5.60 kg/s of air enters a turbine at 800 °C with a velocity of 99 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 148 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.66 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number13EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.47 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 255 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.71 m.<br />Q2) 17.90 kg/s of air enters a turbine at 610 °C with a velocity of 54 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 128 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.73 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number14EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.21 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 395 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.58 m.<br />Q2) 10.20 kg/s of air enters a turbine at 860 °C with a velocity of 75 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 174 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.20 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number15EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.25 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 355 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.67 m.<br />Q2) 12.80 kg/s of air enters a turbine at 1150 °C with a velocity of 84 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 160 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.58 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number16EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.50 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 335 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.63 m.<br />Q2) 9.30 kg/s of air enters a turbine at 1080 °C with a velocity of 75 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 164 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.20 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number17EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.46 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 385 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.36 m.<br />Q2) 19.80 kg/s of air enters a turbine at 640 °C with a velocity of 90 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 110 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.00 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number18EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.47 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 295 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.54 m.<br />Q2) 15.20 kg/s of air enters a turbine at 690 °C with a velocity of 64 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 112 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 5.00 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number19EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.43 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 215 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42 m.<br />Q2) 9.80 kg/s of air enters a turbine at 540 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 112 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.94 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number20EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.31 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 330 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.46 m.<br />Q2) 16.30 kg/s of air enters a turbine at 680 °C with a velocity of 84 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 120 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.86 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number21EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.50 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 430 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.47 m.<br />Q2) 6.30 kg/s of air enters a turbine at 940 °C with a velocity of 79 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 168 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.54 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number22EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.28 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 290 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.69 m.<br />Q2) 6.60 kg/s of air enters a turbine at 950 °C with a velocity of 52 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 124 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.99 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number23EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 340 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.64 m.<br />Q2) 12.00 kg/s of air enters a turbine at 670 °C with a velocity of 98 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 166 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.58 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number24EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.21 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 395 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.36 m.<br />Q2) 5.60 kg/s of air enters a turbine at 1200 °C with a velocity of 74 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 124 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.35 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number25EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.47 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 340 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.31 m.<br />Q2) 14.90 kg/s of air enters a turbine at 1070 °C with a velocity of 88 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 178 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.67 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number26EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.25 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 365 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.65 m.<br />Q2) 5.30 kg/s of air enters a turbine at 620 °C with a velocity of 72 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.23 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number27EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.27 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 320 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.41 m.<br />Q2) 13.10 kg/s of air enters a turbine at 840 °C with a velocity of 82 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 166 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.14 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number28EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.20 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 365 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.68 m.<br />Q2) 12.00 kg/s of air enters a turbine at 510 °C with a velocity of 74 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 126 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.50 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number29EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 385 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.35 m.<br />Q2) 12.80 kg/s of air enters a turbine at 850 °C with a velocity of 96 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 176 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.73 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number30EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.41 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 245 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.52 m.<br />Q2) 16.60 kg/s of air enters a turbine at 770 °C with a velocity of 59 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 132 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.67 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number31EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.27 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 395 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.62 m.<br />Q2) 15.60 kg/s of air enters a turbine at 750 °C with a velocity of 89 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 140 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.01 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number32EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.35 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 375 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.33 m.<br />Q2) 13.30 kg/s of air enters a turbine at 830 °C with a velocity of 77 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 160 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.71 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number33EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.21 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 300 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.46 m.<br />Q2) 9.60 kg/s of air enters a turbine at 650 °C with a velocity of 78 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 118 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.53 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number34EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.30 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 260 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.61 m.<br />Q2) 7.50 kg/s of air enters a turbine at 670 °C with a velocity of 68 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 134 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.59 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number35EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 320 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.69 m.<br />Q2) 8.30 kg/s of air enters a turbine at 860 °C with a velocity of 74 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 122 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.79 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number36EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.33 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 235 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.60 m.<br />Q2) 12.60 kg/s of air enters a turbine at 670 °C with a velocity of 58 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 170 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.53 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number37EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 395 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.67 m.<br />Q2) 19.90 kg/s of air enters a turbine at 1100 °C with a velocity of 73 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 122 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.86 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number38EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.35 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 230 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.75 m.<br />Q2) 19.60 kg/s of air enters a turbine at 950 °C with a velocity of 53 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 156 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.13 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number39EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.34 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 245 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.33 m.<br />Q2) 18.50 kg/s of air enters a turbine at 620 °C with a velocity of 66 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 114 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 2.84 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number40EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.46 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 310 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.38 m.<br />Q2) 16.40 kg/s of air enters a turbine at 800 °C with a velocity of 56 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 114 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.10 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number41EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.26 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 445 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.42 m.<br />Q2) 10.80 kg/s of air enters a turbine at 580 °C with a velocity of 60 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 154 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.00 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number42EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.23 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 340 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.44 m.<br />Q2) 10.90 kg/s of air enters a turbine at 1180 °C with a velocity of 90 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 174 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.82 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number43EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.44 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 345 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.79 m.<br />Q2) 14.80 kg/s of air enters a turbine at 970 °C with a velocity of 53 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 124 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.74 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number44EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.40 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 395 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.39 m.<br />Q2) 11.60 kg/s of air enters a turbine at 1050 °C with a velocity of 91 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.66 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number45EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 300 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.33 m.<br />Q2) 14.10 kg/s of air enters a turbine at 530 °C with a velocity of 87 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 134 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.22 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number46EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.20 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 5 bars. Heat is added until the final temperature is 275 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.70 m.<br />Q2) 13.80 kg/s of air enters a turbine at 880 °C with a velocity of 53 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 166 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.02 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number47EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.29 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 7 bars. Heat is added until the final temperature is 435 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.60 m.<br />Q2) 19.40 kg/s of air enters a turbine at 1100 °C with a velocity of 99 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 130 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.81 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number48EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.44 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 325 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.48 m.<br />Q2) 18.00 kg/s of air enters a turbine at 720 °C with a velocity of 95 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 118 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 4.09 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number49EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.39 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 8 bars. Heat is added until the final temperature is 270 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.43 m.<br />Q2) 14.40 kg/s of air enters a turbine at 850 °C with a velocity of 94 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 110 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.26 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Fluid Mechanics and Thermodynamics.<br />Weekly Assessed Tutorial Sheet 10.<br />Student Number50EENameHand out dateHand in date<br />Q1). A cylinder of diameter 0.35 m, fitted with a gas tight, frictionless piston contains dry saturated steam at 6 bars. Heat is added until the final temperature is 310 ° C. Determine <br />i) the work done (kJ) [3 dp](2 marks)<br />ii) the heat supplied (kJ)[2 dp](1 mark)<br />iii) the change in internal energy (kJ). [2 dp](2 marks)<br />You may assume that the piston is free to rise as a consequence of any expansion and at the start of the process the distance between the piston and the bottom of the cylinder is 0.75 m.<br />Q2) 7.80 kg/s of air enters a turbine at 580 °C with a velocity of 88 m/s. The air expands adiabatically as it passes through the turbine and leaves with a velocity of 136 m/s. It then enters a diffuser where the velocity is reduced to a negligible value. If the turbine produces 3.45 MW calculate <br />i) The temperature of the air at exit from the turbine (C)[1 dp](3 marks)<br />ii)The temperature of the air at exit from the diffuser (C)[1 dp](3 marks)<br />You may assume that the Cp for air is constant and has a value of 1.005 kJ/kg K.<br />Credits<br />This resource was created by the University of Hertfordshire and released as an open educational resource through the Open Engineering Resources project of the HE Academy Engineering Subject Centre. The Open Engineering Resources project was funded by HEFCE and part of the JISC/HE Academy UKOER programme.<br />© University of Hertfordshire 2009<br />This work is licensed under a Creative Commons Attribution 2.0 License. <br />The name of the University of Hertfordshire, UH and the UH logo are the name and registered marks of the University of Hertfordshire. To the fullest extent permitted by law the University of Hertfordshire reserves all its rights in its name and marks which may not be used except with its written permission.<br />The JISC logo is licensed under the terms of the Creative Commons Attribution-Non-Commercial-No Derivative Works 2.0 UK: England & Wales Licence.  All reproductions must comply with the terms of that licence.<br />The HEA logo is owned by the Higher Education Academy Limited may be freely distributed and copied for educational purposes only, provided that appropriate acknowledgement is given to the Higher Education Academy as the copyright holder and original publisher.<br />