SlideShare uma empresa Scribd logo
1 de 32
Baixar para ler offline
6/19/2015 1Hareesha N G, Dept of Aero Engg, DSCE, Blore
Unit 1: Static Force Analysis
• Static force analysis
– Introduction
– Static equilibrium
– Equilibrium of two and three force members
– Members with two forces and torque
– Free body diagrams
– principle of virtual work
• Static force analysis of
– four bar mechanism
– slider-crank mechanism with and without friction.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 2
STATIC EQUILIBRIUM
• A body is in static equilibrium if it remains in its state of rest or
motion.
• If the body is at rest, it tends to remain at rest and if in motion, it
tends to keep the motion.
• In static equilibrium,
– the vector sum of all the forces acting on the body is zero and
– the vector sum of all the moments about any arbitrary point is zero.
• Mathematically,
• In a planer system, forces can be described by two-dimensional
vectors and therefore,
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 3
EQUILIBRIUM OF TWO AND THREE-FORCE MEMBERS
• A member under the action of two forces will be in
equilibrium if
– the forces are of the same magnitude,
– the forces act along the same line, and
– the forces are in opposite directions.
• Figure shows such a member.
• A member under the action of three forces will be in
equilibrium if
– the resultant of the forces is zero, and
– the lines of action of the forces intersect at a point (known as
point of concurrency).
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 4
EQUILIBRIUM OF TWO AND THREE-FORCE MEMBERS (Contd….)
• Figure (a) shows a member acted upon by three forces F1, F2 and F3
and is in equilibrium as the lines of action of forces intersect at one
point O and the resultant is zero.
• This is verified by adding the forces vectorially [Fig.(b)].
• As the head of the last vector F3 meets the tail of the first vector F1,
the resultant is zero.
• Figure (d) shows a case where the magnitudes and directions of the
forces are the same as before, but the lines of action of the forces do
not intersect at one point.
• Thus, the member is not in equilibrium.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 5
• Consider a member in equilibrium in which force F1 is completely
known, F2 known in direction only and F3 completely unknown.
• The point of applications of F1 , F2 and F3 are A, B and C respectively.
• To solve such a problem, first find the point of concurrency O from the
two forces with known directions, i.e. from F1, and F2.
• Joining O with C gives the line of action of the third force F3.
• To know the magnitudes of the forces F2 and F3, take a vector of proper
magnitude and direction to represent the force F1.
• From its two ends, draw lines parallel to lines of action of the forces F2
and F3 forming a force triangle [Fig.].
• Mark arrowheads on F2 and F3 so that F1 , F2 and F3 are in the same
order.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 6
MEMBER WITH TWO FORCES AND A TORQUE
• A member under the action of two forces and an applied torque will
be in equilibrium if
– the forces are equal in magnitude, parallel in direction and opposite in sense
and
– the forces form a couple which is equal and opposite to the applied torque.
• Figure shows a member acted upon by two equal forces F1, and F2
and an applied torque T for equilibrium,
where T, F1 and F2 are the magnitudes of T, F1 and F2 respectively.
• T is clockwise whereas the couple formed by F1, and F2 is counter-
clockwise.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 7
FORCE CONVENTION
• The force exerted by member i on member j is represented
by Fij
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 8
FREE BODY DIAGRAMS
• A free body diagram is a sketch or diagram of a part isolated from the
mechanism in order to determine the nature of forces acting on it.
• Figure (a) shows a four-link mechanism.
• The free-body diagrams of its members 2, 3 and 4 are shown in Figs.
(b), (c) and (d) respectively.
• Various forces acting on each member are also shown.
• As the mechanism is in static equilibrium, each of its members must
be in equilibrium individually.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 9
• Member 4 is acted upon by three forces F, F34 and F14.
• Member 3 is acted upon by two forces F23 and F43
• Member 2 is acted upon by two forces F32 and F12 and a torque T.
• Initially, the direction and the sense of some of the forces may not be
known.
• Link 3 is a two-force member and for its equilibrium F23 and F43 must
act along BC.
• Thus, F34 being equal and opposite to F43 also acts along BC.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 10
• Assume that the force F on member 4 is known completely.
• To know the other two forces acting on this member completely, the
direction of one more force must be known.
• For member 4 to be in equilibrium, F14 passes through the intersection
of F and F34 .
• By drawing a force triangle (F is completely known), magnitudes of
F14 and F34 can be known [Fig.(e)].
Now F34 = F43 = F23 = F32
• Member 2 will be in equilibrium if F12 is equal, parallel and opposite
to F32 and
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 11
A four-link mechanism with the following dimensions is acted upon by
a force 80N at angle 1500 on link DC [Fig.(a)): AD = 50 mm, AB = 40 mm,
BC = 100 mm, DC = 75 mm, DE = 35 mm. Determine the input torque T
on the link AB for the static equilibrium of the mechanism for the given
configuration.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 12
As the mechanism is in static equilibrium, each of its
members must also be in equilibrium individually.
Member 4 is acted upon by three forces F F34 and F14.
Member 3 is acted upon by two forces F23 and F43
Member 2 is acted upon by two forces F32 and F12 and
a torque T.
Initially, the direction and the sense of some of the
forces are not known.
Force F on member 4 is known completely. To know the other two forces acting
on this member completely, the direction of one more force must be known. To
know that, link 3 will have to be considered first which is a two-force member.
• As link 3 is a two-force member [Fig.(b)], for its equilibrium, F23 and
F43 must act along BC (at this stage, the sense of direction of forces F23
and F43 is not known). Thus, the line of action of F34 is also along BC.
• As force F34 acts through point C on link 4, draw a line parallel to BC
through C by taking a free body of link 4 to represent the same. Now,
as link 4 is three force member, the third force F14 passes through the
intersection of F and F34 [Fig (c)].
• By drawing a force triangle (F is completely known), magnitudes of
F14 and F34 are known [Fig(d)].
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 13
From force triangle, F34 = 47.8 N
• Now, F34 = -F43 =F23 = -F32
• Member 2 will be in equilibrium [Fig. (e)] if F12 is equal, parallel and
opposite to F32 and
T=-F32 x h = 47.8 x 39.3 = -1878.54 N.mm The input torque has to be
equal and opposite to this couple i.e. T= 1878.5 N/mm (clockwise)
h=Perpendicular distance between two equal and opposite forces.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 14
Figure shows a slider crank mechanism in which the resultant gas pressure 8x104 N/m2
acts on the piston of cross sectional area 0.1m2 The system is kept in equilibrium as a
result of the couple applied to the crank 2, through the shaft at O2. Determine forces
acting on all the links (including the pins) and the couple on 2. OA=100mm, AB=450mm.
6/19/2015
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
15
6/19/2015
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
16
Force triangle for the forces acting on(4)is drawn to some suitable scale.
Magnitude and direction of P known and lines of action of F34 & F14
known.
Measure the lengths of vectors and multiply by the scale factor to get the magnitudes
of F14 & F34.
Directions are also fixed.
Since link 3 is acted upon by only two forces, F43 and F23
are collinear, equal in magnitude and opposite in direction
i.e., F43 = -F23 =8.8xl03 N
Also, F23 = - F32 (equal in magnitude and opposite in
direction).
6/19/2015
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
17
Link 2 is acted upon by 2 forces and a torque, for equilibrium
the two forces must be equal, parallel and opposite and their
sense must be opposite to T2.
There fore,
F32 = -F12 =8.8xl03 N
F32 & F12 form a counter clock wise couple of magnitude,
F23 * h = F12 *h
=(8.8xl03)x0.125 = 1100 Nm.
To keep 2 in equilibrium, T: should act clockwise and
magnitude is 1100 Nm.
Note: h is measured perpendicular to F32 &F12
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 18
For the static equilibrium of the quick return mechanism shown in Fig (a), determine the input
torque T2: to be applied on link AB Tor a force of 300N on the slider D. The dimensions of the
various links arc OA=400mm, AB=200mm, OC=800mm. CD=300mm
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 19
• For the mechanism shown in Fig., determine the torque on the link
AB for the static equilibrium of the mechanism.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 20
• Answers from Composite Graphical Solution
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 21
Graphical Solution by Superposition method
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 22
Graphical Solution by Superposition method
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 23
In a four-link mechanism shown in Fig., torque T3 and T4 have
magnitudes of 30N.m and2 ON. m respectively. The link lengths are AD
= 800 mm, AB = 300 mm, BC = 700 mm and CD = 400 mm. For the static
equilibrium of the mechanism, determine the required input torque T2
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 24
In a four-link mechanism shown in Fig., torque T3 and T4 have
magnitudes of 30N.m and2 ON. m respectively. The link lengths are AD
= 800 mm, AB = 300 mm, BC = 700 mm and CD = 400 mm. For the static
equilibrium of the mechanism, determine the required input torque T2
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 25
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 26
Neglecting torque T3
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 27
Neglecting torque T4
PRINCIPLE OF VIRTUAL WORK
• The principle of virtual (imaginary) work can be stated
as the work done during a virtual displacement from the
equilibrium is equal to zero.
• Virtual displacement may be defined as an imaginary
infinitesimal displacement of the system.
• By applying this principle, an entire mechanism is
examined as a whole and there is no need of dividing it
into free bodies.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 28
• Consider a slider-crank mechanism shown in Fig.
• It is acted upon by the external piston force F, the external
crankshaft torque T and the force at the bearings.
• As the crank rotates through a small angular displacement
δθ, the corresponding displacement of the piston is δx, the
various forces acting on the system are
– Bearing reaction at O (performs no work)
– Force of cylinder on piston, perpendicular to piston
displacement (produces no work)
– Bearing forces at A and B, being equal and opposite (AB is a
two-force member), no work is done
– Work done by torque T= T δθ
– Work done by force F = F δx
• Work done is positive if a force acts in the direction of the
displacement and negative if it acts in the opposite
direction.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 29
The negative sign indicates that for equilibrium, T must be applied in
the opposite direction to the angular displacement.
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 30
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 31
6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 32

Mais conteúdo relacionado

Mais procurados

Theory of machine
Theory of machine Theory of machine
Theory of machine ahirehemant
 
Unit 1 Metal Cutting
Unit 1 Metal CuttingUnit 1 Metal Cutting
Unit 1 Metal CuttingMechbytes
 
Turning Moment Diagram and Flywheel
Turning Moment Diagram and FlywheelTurning Moment Diagram and Flywheel
Turning Moment Diagram and FlywheelRonak Soni
 
Mechanical Vibrations all slides
Mechanical Vibrations all slidesMechanical Vibrations all slides
Mechanical Vibrations all slidesEbrahim Hanash
 
Unit 3 design against fluctuation load
Unit 3 design against fluctuation loadUnit 3 design against fluctuation load
Unit 3 design against fluctuation loadSomnath Kolgiri
 
Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...
Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...
Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...Jay Patel
 
Springs - DESIGN OF MACHINE ELEMENTS-II
Springs - DESIGN OF MACHINE ELEMENTS-IISprings - DESIGN OF MACHINE ELEMENTS-II
Springs - DESIGN OF MACHINE ELEMENTS-IIDr. L K Bhagi
 
design of Brakes system
design of Brakes  systemdesign of Brakes  system
design of Brakes systemashok184924
 
Module 1 introduction to kinematics of machinery
Module 1 introduction to kinematics of machineryModule 1 introduction to kinematics of machinery
Module 1 introduction to kinematics of machinerytaruian
 
Theory of machines by rs. khurmi_ solution manual _ chapter 7
Theory of machines by rs. khurmi_ solution manual _ chapter 7Theory of machines by rs. khurmi_ solution manual _ chapter 7
Theory of machines by rs. khurmi_ solution manual _ chapter 7Darawan Wahid
 
Theory of machines solution of exercise
Theory of machines solution of exerciseTheory of machines solution of exercise
Theory of machines solution of exerciseSaif al-din ali
 
FOUR BAR CHAIN AND INVERSIONS
FOUR BAR CHAIN AND INVERSIONSFOUR BAR CHAIN AND INVERSIONS
FOUR BAR CHAIN AND INVERSIONSsaahil kshatriya
 
Chip formation and types
Chip formation and typesChip formation and types
Chip formation and typesKANNANS94
 

Mais procurados (20)

Theory of machine
Theory of machine Theory of machine
Theory of machine
 
Unit 1 Metal Cutting
Unit 1 Metal CuttingUnit 1 Metal Cutting
Unit 1 Metal Cutting
 
Turning Moment Diagram and Flywheel
Turning Moment Diagram and FlywheelTurning Moment Diagram and Flywheel
Turning Moment Diagram and Flywheel
 
Turning moment-diagram-flywheel
Turning moment-diagram-flywheelTurning moment-diagram-flywheel
Turning moment-diagram-flywheel
 
DYNAMICS OF MACHINES UNIT-1 BY Mr.P.RAMACHANDRAN/AP/MECH/KIT/CBE
DYNAMICS OF MACHINES UNIT-1 BY Mr.P.RAMACHANDRAN/AP/MECH/KIT/CBEDYNAMICS OF MACHINES UNIT-1 BY Mr.P.RAMACHANDRAN/AP/MECH/KIT/CBE
DYNAMICS OF MACHINES UNIT-1 BY Mr.P.RAMACHANDRAN/AP/MECH/KIT/CBE
 
Mechanical Vibrations all slides
Mechanical Vibrations all slidesMechanical Vibrations all slides
Mechanical Vibrations all slides
 
Gear trains
Gear trainsGear trains
Gear trains
 
Unit 3 design against fluctuation load
Unit 3 design against fluctuation loadUnit 3 design against fluctuation load
Unit 3 design against fluctuation load
 
Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...
Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...
Parson’s Turbine and condition for maximum efficiency of Parson’s reaction Tu...
 
Springs - DESIGN OF MACHINE ELEMENTS-II
Springs - DESIGN OF MACHINE ELEMENTS-IISprings - DESIGN OF MACHINE ELEMENTS-II
Springs - DESIGN OF MACHINE ELEMENTS-II
 
Gyroscope
GyroscopeGyroscope
Gyroscope
 
design of Brakes system
design of Brakes  systemdesign of Brakes  system
design of Brakes system
 
Design of Springs
Design of SpringsDesign of Springs
Design of Springs
 
Module 1 introduction to kinematics of machinery
Module 1 introduction to kinematics of machineryModule 1 introduction to kinematics of machinery
Module 1 introduction to kinematics of machinery
 
Bevel gears
Bevel gearsBevel gears
Bevel gears
 
Theory of machines by rs. khurmi_ solution manual _ chapter 7
Theory of machines by rs. khurmi_ solution manual _ chapter 7Theory of machines by rs. khurmi_ solution manual _ chapter 7
Theory of machines by rs. khurmi_ solution manual _ chapter 7
 
Unit 4 helical gear
Unit 4 helical gearUnit 4 helical gear
Unit 4 helical gear
 
Theory of machines solution of exercise
Theory of machines solution of exerciseTheory of machines solution of exercise
Theory of machines solution of exercise
 
FOUR BAR CHAIN AND INVERSIONS
FOUR BAR CHAIN AND INVERSIONSFOUR BAR CHAIN AND INVERSIONS
FOUR BAR CHAIN AND INVERSIONS
 
Chip formation and types
Chip formation and typesChip formation and types
Chip formation and types
 

Destaque (8)

Speed Governers
Speed GovernersSpeed Governers
Speed Governers
 
Friction and belt drives
Friction and belt drivesFriction and belt drives
Friction and belt drives
 
Energy Conversion Engineering Laboratory Manual
Energy Conversion Engineering Laboratory ManualEnergy Conversion Engineering Laboratory Manual
Energy Conversion Engineering Laboratory Manual
 
brakes and dynamometer
brakes and dynamometerbrakes and dynamometer
brakes and dynamometer
 
Design and Drawing of CAM profiles
Design and Drawing of CAM profilesDesign and Drawing of CAM profiles
Design and Drawing of CAM profiles
 
Planar Mechanisms
Planar MechanismsPlanar Mechanisms
Planar Mechanisms
 
Introduction to Mechanisms
Introduction to MechanismsIntroduction to Mechanisms
Introduction to Mechanisms
 
Velocity and acceleration of mechanisms
Velocity and acceleration of mechanismsVelocity and acceleration of mechanisms
Velocity and acceleration of mechanisms
 

Semelhante a Static Force Analysis

Unit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanismUnit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanismMatam Prasad
 
Unit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanismUnit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanismMatam Prasad
 
EDC-PPT.pptx
EDC-PPT.pptxEDC-PPT.pptx
EDC-PPT.pptxsanjay bs
 
B6 force-analysis-of-machinery-slide
B6 force-analysis-of-machinery-slideB6 force-analysis-of-machinery-slide
B6 force-analysis-of-machinery-slideMatam Prasad
 
force analysis in civil engineering force
force analysis in civil engineering forceforce analysis in civil engineering force
force analysis in civil engineering forceDr. Karrar Alwash
 
engineering statics :force systems
 engineering statics :force systems engineering statics :force systems
engineering statics :force systemsmusadoto
 
14. space forces
14. space forces14. space forces
14. space forcesEkeeda
 
Space Forces
Space ForcesSpace Forces
Space ForcesEkeeda
 
Space forces
Space forcesSpace forces
Space forcesEkeeda
 
Chapter 2: Two dimenstional force systems: DBU-MESA
Chapter 2:  Two dimenstional  force systems: DBU-MESAChapter 2:  Two dimenstional  force systems: DBU-MESA
Chapter 2: Two dimenstional force systems: DBU-MESAYitagesu Ethiopia
 
2.9 analysing forces in equilibrium
2.9 analysing forces in equilibrium2.9 analysing forces in equilibrium
2.9 analysing forces in equilibriumNurul Fadhilah
 
Lecture Statics Moments of Forces
Lecture Statics Moments of ForcesLecture Statics Moments of Forces
Lecture Statics Moments of ForcesNikolai Priezjev
 
module 2 (Mechanics)
module 2 (Mechanics)module 2 (Mechanics)
module 2 (Mechanics)Nexus
 

Semelhante a Static Force Analysis (20)

Unit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanismUnit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanism
 
Unit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanismUnit 1-staticforceanalysis of slider crank and four bar mechanism
Unit 1-staticforceanalysis of slider crank and four bar mechanism
 
Forceanalysis
ForceanalysisForceanalysis
Forceanalysis
 
EDC-PPT.pptx
EDC-PPT.pptxEDC-PPT.pptx
EDC-PPT.pptx
 
B6 force-analysis-of-machinery-slide
B6 force-analysis-of-machinery-slideB6 force-analysis-of-machinery-slide
B6 force-analysis-of-machinery-slide
 
Resultant of forces
Resultant of forcesResultant of forces
Resultant of forces
 
force analysis in civil engineering force
force analysis in civil engineering forceforce analysis in civil engineering force
force analysis in civil engineering force
 
Force system
Force systemForce system
Force system
 
engineering statics :force systems
 engineering statics :force systems engineering statics :force systems
engineering statics :force systems
 
14. space forces
14. space forces14. space forces
14. space forces
 
Space Forces
Space ForcesSpace Forces
Space Forces
 
Space forces
Space forcesSpace forces
Space forces
 
visual aids
visual aidsvisual aids
visual aids
 
Chapter 2: Two dimenstional force systems: DBU-MESA
Chapter 2:  Two dimenstional  force systems: DBU-MESAChapter 2:  Two dimenstional  force systems: DBU-MESA
Chapter 2: Two dimenstional force systems: DBU-MESA
 
Lecture 2 kosygin
Lecture 2 kosyginLecture 2 kosygin
Lecture 2 kosygin
 
2.9 analysing forces in equilibrium
2.9 analysing forces in equilibrium2.9 analysing forces in equilibrium
2.9 analysing forces in equilibrium
 
Mechanics 3
Mechanics 3Mechanics 3
Mechanics 3
 
Lecture Statics Moments of Forces
Lecture Statics Moments of ForcesLecture Statics Moments of Forces
Lecture Statics Moments of Forces
 
module 2 (Mechanics)
module 2 (Mechanics)module 2 (Mechanics)
module 2 (Mechanics)
 
3 analysis
3 analysis3 analysis
3 analysis
 

Mais de Hareesha N Gowda, Dayananda Sagar College of Engg, Bangalore

Mais de Hareesha N Gowda, Dayananda Sagar College of Engg, Bangalore (20)

Alumni Meet Invitation.pdf
Alumni Meet Invitation.pdfAlumni Meet Invitation.pdf
Alumni Meet Invitation.pdf
 
Brammadevarahalli GP Panchapayana
Brammadevarahalli GP PanchapayanaBrammadevarahalli GP Panchapayana
Brammadevarahalli GP Panchapayana
 
Introduction to control systems
Introduction to control systemsIntroduction to control systems
Introduction to control systems
 
Be project report template
Be project report templateBe project report template
Be project report template
 
Computer aided machine drawing manual
Computer aided machine drawing manualComputer aided machine drawing manual
Computer aided machine drawing manual
 
Unit 1- simple stress and strain
Unit 1- simple stress and strainUnit 1- simple stress and strain
Unit 1- simple stress and strain
 
Unit 8: Torsion of circular shafts and elastic stability of columns
Unit 8: Torsion of circular shafts and elastic stability of columnsUnit 8: Torsion of circular shafts and elastic stability of columns
Unit 8: Torsion of circular shafts and elastic stability of columns
 
Unit 6: Bending and shear Stresses in beams
Unit 6: Bending and shear Stresses in beamsUnit 6: Bending and shear Stresses in beams
Unit 6: Bending and shear Stresses in beams
 
Unit 5 shear force and bending moment in beams
Unit 5  shear force and bending moment in beamsUnit 5  shear force and bending moment in beams
Unit 5 shear force and bending moment in beams
 
Unit 3 Compound stresses
Unit 3  Compound stressesUnit 3  Compound stresses
Unit 3 Compound stresses
 
Unit 2 stresses in composite sections
Unit 2  stresses in composite sectionsUnit 2  stresses in composite sections
Unit 2 stresses in composite sections
 
Dynamics of Machines: Question bank unitwise from vtu old question papers
Dynamics of Machines: Question bank unitwise from vtu old question papersDynamics of Machines: Question bank unitwise from vtu old question papers
Dynamics of Machines: Question bank unitwise from vtu old question papers
 
Mechanics of Materials: Question Bank from old VTU Question papers
Mechanics of Materials: Question Bank from old VTU Question papersMechanics of Materials: Question Bank from old VTU Question papers
Mechanics of Materials: Question Bank from old VTU Question papers
 
Robots: state of-the-art and future trends
Robots: state of-the-art and future trendsRobots: state of-the-art and future trends
Robots: state of-the-art and future trends
 
Screw thread measurements and Gear measurement
Screw thread measurements and Gear measurementScrew thread measurements and Gear measurement
Screw thread measurements and Gear measurement
 
Force, Pressure and Torque measurements
Force, Pressure and Torque measurementsForce, Pressure and Torque measurements
Force, Pressure and Torque measurements
 
Mechanical measurements and Measurement systems
Mechanical measurements and Measurement systemsMechanical measurements and Measurement systems
Mechanical measurements and Measurement systems
 
CIM and automation laboratory manual
CIM and automation laboratory manualCIM and automation laboratory manual
CIM and automation laboratory manual
 
Introduction to Non-Traditional Machining
Introduction to Non-Traditional MachiningIntroduction to Non-Traditional Machining
Introduction to Non-Traditional Machining
 
Chemical machining
Chemical machiningChemical machining
Chemical machining
 

Último

Paris 2024 Olympic Geographies - an activity
Paris 2024 Olympic Geographies - an activityParis 2024 Olympic Geographies - an activity
Paris 2024 Olympic Geographies - an activityGeoBlogs
 
Introduction to Nonprofit Accounting: The Basics
Introduction to Nonprofit Accounting: The BasicsIntroduction to Nonprofit Accounting: The Basics
Introduction to Nonprofit Accounting: The BasicsTechSoup
 
Student login on Anyboli platform.helpin
Student login on Anyboli platform.helpinStudent login on Anyboli platform.helpin
Student login on Anyboli platform.helpinRaunakKeshri1
 
Activity 01 - Artificial Culture (1).pdf
Activity 01 - Artificial Culture (1).pdfActivity 01 - Artificial Culture (1).pdf
Activity 01 - Artificial Culture (1).pdfciinovamais
 
microwave assisted reaction. General introduction
microwave assisted reaction. General introductionmicrowave assisted reaction. General introduction
microwave assisted reaction. General introductionMaksud Ahmed
 
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.pdfQucHHunhnh
 
BASLIQ CURRENT LOOKBOOK LOOKBOOK(1) (1).pdf
BASLIQ CURRENT LOOKBOOK  LOOKBOOK(1) (1).pdfBASLIQ CURRENT LOOKBOOK  LOOKBOOK(1) (1).pdf
BASLIQ CURRENT LOOKBOOK LOOKBOOK(1) (1).pdfSoniaTolstoy
 
fourth grading exam for kindergarten in writing
fourth grading exam for kindergarten in writingfourth grading exam for kindergarten in writing
fourth grading exam for kindergarten in writingTeacherCyreneCayanan
 
APM Welcome, APM North West Network Conference, Synergies Across Sectors
APM Welcome, APM North West Network Conference, Synergies Across SectorsAPM Welcome, APM North West Network Conference, Synergies Across Sectors
APM Welcome, APM North West Network Conference, Synergies Across SectorsAssociation for Project Management
 
Key note speaker Neum_Admir Softic_ENG.pdf
Key note speaker Neum_Admir Softic_ENG.pdfKey note speaker Neum_Admir Softic_ENG.pdf
Key note speaker Neum_Admir Softic_ENG.pdfAdmir Softic
 
Holdier Curriculum Vitae (April 2024).pdf
Holdier Curriculum Vitae (April 2024).pdfHoldier Curriculum Vitae (April 2024).pdf
Holdier Curriculum Vitae (April 2024).pdfagholdier
 
Arihant handbook biology for class 11 .pdf
Arihant handbook biology for class 11 .pdfArihant handbook biology for class 11 .pdf
Arihant handbook biology for class 11 .pdfchloefrazer622
 
Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...
Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...
Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...fonyou31
 
Measures of Dispersion and Variability: Range, QD, AD and SD
Measures of Dispersion and Variability: Range, QD, AD and SDMeasures of Dispersion and Variability: Range, QD, AD and SD
Measures of Dispersion and Variability: Range, QD, AD and SDThiyagu K
 
9548086042 for call girls in Indira Nagar with room service
9548086042  for call girls in Indira Nagar  with room service9548086042  for call girls in Indira Nagar  with room service
9548086042 for call girls in Indira Nagar with room servicediscovermytutordmt
 
Grant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy ConsultingGrant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy ConsultingTechSoup
 
Software Engineering Methodologies (overview)
Software Engineering Methodologies (overview)Software Engineering Methodologies (overview)
Software Engineering Methodologies (overview)eniolaolutunde
 
Accessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impactAccessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impactdawncurless
 

Último (20)

Paris 2024 Olympic Geographies - an activity
Paris 2024 Olympic Geographies - an activityParis 2024 Olympic Geographies - an activity
Paris 2024 Olympic Geographies - an activity
 
Código Creativo y Arte de Software | Unidad 1
Código Creativo y Arte de Software | Unidad 1Código Creativo y Arte de Software | Unidad 1
Código Creativo y Arte de Software | Unidad 1
 
Introduction to Nonprofit Accounting: The Basics
Introduction to Nonprofit Accounting: The BasicsIntroduction to Nonprofit Accounting: The Basics
Introduction to Nonprofit Accounting: The Basics
 
Student login on Anyboli platform.helpin
Student login on Anyboli platform.helpinStudent login on Anyboli platform.helpin
Student login on Anyboli platform.helpin
 
Activity 01 - Artificial Culture (1).pdf
Activity 01 - Artificial Culture (1).pdfActivity 01 - Artificial Culture (1).pdf
Activity 01 - Artificial Culture (1).pdf
 
microwave assisted reaction. General introduction
microwave assisted reaction. General introductionmicrowave assisted reaction. General introduction
microwave assisted reaction. General introduction
 
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
 
BASLIQ CURRENT LOOKBOOK LOOKBOOK(1) (1).pdf
BASLIQ CURRENT LOOKBOOK  LOOKBOOK(1) (1).pdfBASLIQ CURRENT LOOKBOOK  LOOKBOOK(1) (1).pdf
BASLIQ CURRENT LOOKBOOK LOOKBOOK(1) (1).pdf
 
fourth grading exam for kindergarten in writing
fourth grading exam for kindergarten in writingfourth grading exam for kindergarten in writing
fourth grading exam for kindergarten in writing
 
APM Welcome, APM North West Network Conference, Synergies Across Sectors
APM Welcome, APM North West Network Conference, Synergies Across SectorsAPM Welcome, APM North West Network Conference, Synergies Across Sectors
APM Welcome, APM North West Network Conference, Synergies Across Sectors
 
Key note speaker Neum_Admir Softic_ENG.pdf
Key note speaker Neum_Admir Softic_ENG.pdfKey note speaker Neum_Admir Softic_ENG.pdf
Key note speaker Neum_Admir Softic_ENG.pdf
 
Holdier Curriculum Vitae (April 2024).pdf
Holdier Curriculum Vitae (April 2024).pdfHoldier Curriculum Vitae (April 2024).pdf
Holdier Curriculum Vitae (April 2024).pdf
 
Arihant handbook biology for class 11 .pdf
Arihant handbook biology for class 11 .pdfArihant handbook biology for class 11 .pdf
Arihant handbook biology for class 11 .pdf
 
Mattingly "AI & Prompt Design: The Basics of Prompt Design"
Mattingly "AI & Prompt Design: The Basics of Prompt Design"Mattingly "AI & Prompt Design: The Basics of Prompt Design"
Mattingly "AI & Prompt Design: The Basics of Prompt Design"
 
Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...
Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...
Ecosystem Interactions Class Discussion Presentation in Blue Green Lined Styl...
 
Measures of Dispersion and Variability: Range, QD, AD and SD
Measures of Dispersion and Variability: Range, QD, AD and SDMeasures of Dispersion and Variability: Range, QD, AD and SD
Measures of Dispersion and Variability: Range, QD, AD and SD
 
9548086042 for call girls in Indira Nagar with room service
9548086042  for call girls in Indira Nagar  with room service9548086042  for call girls in Indira Nagar  with room service
9548086042 for call girls in Indira Nagar with room service
 
Grant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy ConsultingGrant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy Consulting
 
Software Engineering Methodologies (overview)
Software Engineering Methodologies (overview)Software Engineering Methodologies (overview)
Software Engineering Methodologies (overview)
 
Accessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impactAccessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impact
 

Static Force Analysis

  • 1. 6/19/2015 1Hareesha N G, Dept of Aero Engg, DSCE, Blore
  • 2. Unit 1: Static Force Analysis • Static force analysis – Introduction – Static equilibrium – Equilibrium of two and three force members – Members with two forces and torque – Free body diagrams – principle of virtual work • Static force analysis of – four bar mechanism – slider-crank mechanism with and without friction. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 2
  • 3. STATIC EQUILIBRIUM • A body is in static equilibrium if it remains in its state of rest or motion. • If the body is at rest, it tends to remain at rest and if in motion, it tends to keep the motion. • In static equilibrium, – the vector sum of all the forces acting on the body is zero and – the vector sum of all the moments about any arbitrary point is zero. • Mathematically, • In a planer system, forces can be described by two-dimensional vectors and therefore, 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 3
  • 4. EQUILIBRIUM OF TWO AND THREE-FORCE MEMBERS • A member under the action of two forces will be in equilibrium if – the forces are of the same magnitude, – the forces act along the same line, and – the forces are in opposite directions. • Figure shows such a member. • A member under the action of three forces will be in equilibrium if – the resultant of the forces is zero, and – the lines of action of the forces intersect at a point (known as point of concurrency). 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 4
  • 5. EQUILIBRIUM OF TWO AND THREE-FORCE MEMBERS (Contd….) • Figure (a) shows a member acted upon by three forces F1, F2 and F3 and is in equilibrium as the lines of action of forces intersect at one point O and the resultant is zero. • This is verified by adding the forces vectorially [Fig.(b)]. • As the head of the last vector F3 meets the tail of the first vector F1, the resultant is zero. • Figure (d) shows a case where the magnitudes and directions of the forces are the same as before, but the lines of action of the forces do not intersect at one point. • Thus, the member is not in equilibrium. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 5
  • 6. • Consider a member in equilibrium in which force F1 is completely known, F2 known in direction only and F3 completely unknown. • The point of applications of F1 , F2 and F3 are A, B and C respectively. • To solve such a problem, first find the point of concurrency O from the two forces with known directions, i.e. from F1, and F2. • Joining O with C gives the line of action of the third force F3. • To know the magnitudes of the forces F2 and F3, take a vector of proper magnitude and direction to represent the force F1. • From its two ends, draw lines parallel to lines of action of the forces F2 and F3 forming a force triangle [Fig.]. • Mark arrowheads on F2 and F3 so that F1 , F2 and F3 are in the same order. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 6
  • 7. MEMBER WITH TWO FORCES AND A TORQUE • A member under the action of two forces and an applied torque will be in equilibrium if – the forces are equal in magnitude, parallel in direction and opposite in sense and – the forces form a couple which is equal and opposite to the applied torque. • Figure shows a member acted upon by two equal forces F1, and F2 and an applied torque T for equilibrium, where T, F1 and F2 are the magnitudes of T, F1 and F2 respectively. • T is clockwise whereas the couple formed by F1, and F2 is counter- clockwise. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 7
  • 8. FORCE CONVENTION • The force exerted by member i on member j is represented by Fij 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 8
  • 9. FREE BODY DIAGRAMS • A free body diagram is a sketch or diagram of a part isolated from the mechanism in order to determine the nature of forces acting on it. • Figure (a) shows a four-link mechanism. • The free-body diagrams of its members 2, 3 and 4 are shown in Figs. (b), (c) and (d) respectively. • Various forces acting on each member are also shown. • As the mechanism is in static equilibrium, each of its members must be in equilibrium individually. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 9
  • 10. • Member 4 is acted upon by three forces F, F34 and F14. • Member 3 is acted upon by two forces F23 and F43 • Member 2 is acted upon by two forces F32 and F12 and a torque T. • Initially, the direction and the sense of some of the forces may not be known. • Link 3 is a two-force member and for its equilibrium F23 and F43 must act along BC. • Thus, F34 being equal and opposite to F43 also acts along BC. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 10
  • 11. • Assume that the force F on member 4 is known completely. • To know the other two forces acting on this member completely, the direction of one more force must be known. • For member 4 to be in equilibrium, F14 passes through the intersection of F and F34 . • By drawing a force triangle (F is completely known), magnitudes of F14 and F34 can be known [Fig.(e)]. Now F34 = F43 = F23 = F32 • Member 2 will be in equilibrium if F12 is equal, parallel and opposite to F32 and 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 11
  • 12. A four-link mechanism with the following dimensions is acted upon by a force 80N at angle 1500 on link DC [Fig.(a)): AD = 50 mm, AB = 40 mm, BC = 100 mm, DC = 75 mm, DE = 35 mm. Determine the input torque T on the link AB for the static equilibrium of the mechanism for the given configuration. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 12 As the mechanism is in static equilibrium, each of its members must also be in equilibrium individually. Member 4 is acted upon by three forces F F34 and F14. Member 3 is acted upon by two forces F23 and F43 Member 2 is acted upon by two forces F32 and F12 and a torque T. Initially, the direction and the sense of some of the forces are not known. Force F on member 4 is known completely. To know the other two forces acting on this member completely, the direction of one more force must be known. To know that, link 3 will have to be considered first which is a two-force member.
  • 13. • As link 3 is a two-force member [Fig.(b)], for its equilibrium, F23 and F43 must act along BC (at this stage, the sense of direction of forces F23 and F43 is not known). Thus, the line of action of F34 is also along BC. • As force F34 acts through point C on link 4, draw a line parallel to BC through C by taking a free body of link 4 to represent the same. Now, as link 4 is three force member, the third force F14 passes through the intersection of F and F34 [Fig (c)]. • By drawing a force triangle (F is completely known), magnitudes of F14 and F34 are known [Fig(d)]. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 13 From force triangle, F34 = 47.8 N
  • 14. • Now, F34 = -F43 =F23 = -F32 • Member 2 will be in equilibrium [Fig. (e)] if F12 is equal, parallel and opposite to F32 and T=-F32 x h = 47.8 x 39.3 = -1878.54 N.mm The input torque has to be equal and opposite to this couple i.e. T= 1878.5 N/mm (clockwise) h=Perpendicular distance between two equal and opposite forces. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 14
  • 15. Figure shows a slider crank mechanism in which the resultant gas pressure 8x104 N/m2 acts on the piston of cross sectional area 0.1m2 The system is kept in equilibrium as a result of the couple applied to the crank 2, through the shaft at O2. Determine forces acting on all the links (including the pins) and the couple on 2. OA=100mm, AB=450mm. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 15
  • 16. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 16 Force triangle for the forces acting on(4)is drawn to some suitable scale. Magnitude and direction of P known and lines of action of F34 & F14 known. Measure the lengths of vectors and multiply by the scale factor to get the magnitudes of F14 & F34. Directions are also fixed. Since link 3 is acted upon by only two forces, F43 and F23 are collinear, equal in magnitude and opposite in direction i.e., F43 = -F23 =8.8xl03 N Also, F23 = - F32 (equal in magnitude and opposite in direction).
  • 17. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 17 Link 2 is acted upon by 2 forces and a torque, for equilibrium the two forces must be equal, parallel and opposite and their sense must be opposite to T2. There fore, F32 = -F12 =8.8xl03 N F32 & F12 form a counter clock wise couple of magnitude, F23 * h = F12 *h =(8.8xl03)x0.125 = 1100 Nm. To keep 2 in equilibrium, T: should act clockwise and magnitude is 1100 Nm. Note: h is measured perpendicular to F32 &F12
  • 18. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 18 For the static equilibrium of the quick return mechanism shown in Fig (a), determine the input torque T2: to be applied on link AB Tor a force of 300N on the slider D. The dimensions of the various links arc OA=400mm, AB=200mm, OC=800mm. CD=300mm
  • 19. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 19
  • 20. • For the mechanism shown in Fig., determine the torque on the link AB for the static equilibrium of the mechanism. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 20
  • 21. • Answers from Composite Graphical Solution 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 21
  • 22. Graphical Solution by Superposition method 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 22
  • 23. Graphical Solution by Superposition method 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 23
  • 24. In a four-link mechanism shown in Fig., torque T3 and T4 have magnitudes of 30N.m and2 ON. m respectively. The link lengths are AD = 800 mm, AB = 300 mm, BC = 700 mm and CD = 400 mm. For the static equilibrium of the mechanism, determine the required input torque T2 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 24
  • 25. In a four-link mechanism shown in Fig., torque T3 and T4 have magnitudes of 30N.m and2 ON. m respectively. The link lengths are AD = 800 mm, AB = 300 mm, BC = 700 mm and CD = 400 mm. For the static equilibrium of the mechanism, determine the required input torque T2 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 25
  • 26. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 26 Neglecting torque T3
  • 27. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 27 Neglecting torque T4
  • 28. PRINCIPLE OF VIRTUAL WORK • The principle of virtual (imaginary) work can be stated as the work done during a virtual displacement from the equilibrium is equal to zero. • Virtual displacement may be defined as an imaginary infinitesimal displacement of the system. • By applying this principle, an entire mechanism is examined as a whole and there is no need of dividing it into free bodies. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 28
  • 29. • Consider a slider-crank mechanism shown in Fig. • It is acted upon by the external piston force F, the external crankshaft torque T and the force at the bearings. • As the crank rotates through a small angular displacement δθ, the corresponding displacement of the piston is δx, the various forces acting on the system are – Bearing reaction at O (performs no work) – Force of cylinder on piston, perpendicular to piston displacement (produces no work) – Bearing forces at A and B, being equal and opposite (AB is a two-force member), no work is done – Work done by torque T= T δθ – Work done by force F = F δx • Work done is positive if a force acts in the direction of the displacement and negative if it acts in the opposite direction. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 29
  • 30. The negative sign indicates that for equilibrium, T must be applied in the opposite direction to the angular displacement. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 30
  • 31. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 31
  • 32. 6/19/2015 Hareesha N G, Dept of Aero Engg, DSCE, Blore 32