SlideShare uma empresa Scribd logo
1 de 9
Baixar para ler offline
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
1 | P a g e
PORT FLOW SIMULATION OF AN IC ENGINE
Himanth Kumar H Y,
PG Student
Department of Mechanical Engineering,
Vidyavardhaka College of Engineering, Mysuru, India
Jayashankar N
Associate professor,
Mechanical department,
Vidyavardhaka College of Engineering, Mysuru, India
ABSTRACT
This paper deals with the numerical analysis of 3d model which has inlet port diameter 46mm, valve
diameter 43mm and the length and diameter of the cylinder is 562mm and 93.65mm respectively
which is developed to study the effect of valve lift on the flow of fluid inside the cylinder. For
different valve lifts velocity will change inside the cylinder. Results of CFD simulation indicated that
valve lift affects velocity flow field inside the cylinder. It also proved that CFD is a convenient tool
for designing and optimizing the flow field in the engine.
KEYWORDS-Computational fluid dynamics; intake manifold; inlet port; Numerical simulation;
INTRODUCTION
The internal combustion engine usually consists of four cycles such as intake, compression,
expansion (including combustion) and exhaust. Out of these four processes intake and compression
strokes are most important as these strokes influences the pattern of air flow coming inside cylinder
during intake stroke and it generates the condition needed for the fuel injection during compression
stroke. For maximizing the air passing into the cylinder manifold design has to be optimized. Hence
design of intake manifold is more important in engine design. Experimental methods would cost time
and money to achieve this. Using CFD tool without undergoing any time consuming experiment
engine efficiency can be estimated.
Short discussions of the previous studies of authors are presented here. Chen et.al [1] gives result of
fluid flow through an IC engine inlet port both in experimental and computational mode. The port
was straight generic inlet port. They used CFD tool to analyze the velocity contours near port region.
They have used LDA and LSFV technique to analyze fluid flow. Both experimental and prediction
results shows that the valve lift that affect the flow Robert et.al [2] studied the two common motions
in an automobile engine they are tumble and swirl motion using visualization techniques. Benny et.al
[3] investigates the effect of helical, spiral manifold configuration on air motion in a diesel engine.
Using CFD tool flow patterns of these different manifold configurations are studied. The CFD results
of swirl velocity inside combustion chamber are compared with experimental results.
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
Prasad.et.al [4] investigates the swirl air created due to injecting air into the manifold. To direct air
flow into the inlet manifold they have grooved the inlet manifold with helical groove to create
turbulence in the manifold. The tests are conducted by va
maintained constant.
The main objective of this proje
intake manifold, inlet port and valve
enhances the performance of the engine by improving combustion rate
II MATHEMATICAL FORMULATION
2.1 The physical model and coordinate system
A 3D model of a inlet port and valve with cylinder is s
(Ver. 14.5).
Table 2.1 Dimension
Diameter of
Diameter of the valve
Diameter of the cylinder
Length of the
Valve lift
Fig 2.1 Theoretical model
MESHING
The model is created using ANSYS FLUENT
In-cylinder problems solved in Fluent consist of three stages
geometry into different zones and mesh them properly.
The second stage is to set up the engine case inside Fluent with the help of a setup journal.
The third stage is to perform a transient in
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
VOLUME 2, ISSUE 9, SEP.
sad.et.al [4] investigates the swirl air created due to injecting air into the manifold. To direct air
flow into the inlet manifold they have grooved the inlet manifold with helical groove to create
turbulence in the manifold. The tests are conducted by varying dimensions of groove and speed was
The main objective of this project is to analyze the velocity characteristics of fluid flow through the
intake manifold, inlet port and valve to get optimized swirl and tumble motion, so that one can
enhances the performance of the engine by improving combustion rate.
II MATHEMATICAL FORMULATION
2.1 The physical model and coordinate system
inlet port and valve with cylinder is shown in fig is created in
Table 2.1 Dimensions of various parts of model as shown in Fig 2.1
inlet and outlet port 46 & 39.5 mm
iameter of the valve 43 mm
ameter of the cylinder 93.65 mm
Length of the cylinder 562 mm
Valve lift 10 mm
Theoretical model Geometry model created in fluent
model is created using ANSYS FLUENT software.
solved in Fluent consist of three stages. The first stage is to decompose the
geometry into different zones and mesh them properly.
The second stage is to set up the engine case inside Fluent with the help of a setup journal.
The third stage is to perform a transient in-cylinder simulation.
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
2 | P a g e
sad.et.al [4] investigates the swirl air created due to injecting air into the manifold. To direct air
flow into the inlet manifold they have grooved the inlet manifold with helical groove to create
rying dimensions of groove and speed was
ct is to analyze the velocity characteristics of fluid flow through the
to get optimized swirl and tumble motion, so that one can
is created in ANSYS FLUENT
shown in Fig 2.1
& 39.5 mm
93.65 mm
562 mm
Geometry model created in fluent
first stage is to decompose the
The second stage is to set up the engine case inside Fluent with the help of a setup journal.
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
3 | P a g e
First, the surface is meshed with triangular element. In order to resolve the turbulent boundary layer
on the solid surfaces, it is best to have growing prismatic cells from the Valve surfaces. Finally the
remaining region in the domain is filled with tetrahedral cells. No of elements is used for mesh
generation is 11 to 12 lakhs approximately.
The domain has been subdivided into growing boxes to make it easier to generate the grid. The choice
for the elements has been both tetrahedral and hexahedral mesh volumes.
Fig 3.1 Meshed model in FLUENT
GOVERNING EQUATIONS
There are mainly three equations we solve in computational fluid dynamics problem. They are
Continuity equation, Momentum equation (Navier Stokes equation) and Energy equation.
4.1.1 Continuity Equation
A continuity equation expresses a conservation law by “Equating a net flux over a surface with a loss
or gain of material within the surface”. Continuity equations often can be expressed in either integral
or differential form as shown below.
0=
∂
∂
+ ∫∫ cvcs
dA
t
dAV ρρ
This is a statement of the principle of mass conservation for a steady, one-dimensional flow, with one
inlet and one outlet.
( ) 0=
∂
∂
+∇
t
V
ρ
ρ
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
4 | P a g e
Where,
^^^
k
z
j
y
i
x ∂
∂
+
∂
∂
+
∂
∂
=∇
∂ρ
∂t
+
∂(ρ. u)
∂x
+
∂(ρ. v)
∂y
+
∂(ρ. w)
∂z
= 0
4.1.2 Momentum (Navier Stokes) Equations
The momentum equation is a statement of Newton's Second Law and relates the sum of the forces
acting on an element of fluid to its acceleration or rate of change of momentum. The Newton’s
second law of motion F = ma forms the basis of the momentum equation.
ρ
∂u
∂t
+ ρu
∂u
∂x
+ ρv
∂u
∂y
+ ρw
∂u
∂z
= ρg୶ −
∂p
∂x
+ μ
∂ଶ
u
∂xଶ
+ μ
∂ଶ
u
∂yଶ
+ μ
∂ଶ
u
∂zଶ
ρ
∂v
∂t
+ ρu
∂v
∂x
+ ρv
∂v
∂y
+ ρw
∂v
∂z
= ρg୷ −
∂p
∂y
+ μ
∂ଶ
v
∂xଶ
+ μ
∂ଶ
v
∂yଶ
+ μ
∂ଶ
v
∂zଶ
ρ
∂w
∂t
+ ρu
∂w
∂x
+ ρv
∂w
∂y
+ ρw
∂w
∂z
= ρg୸ −
∂p
∂z
+ μ
∂ଶ
w
∂xଶ
+ μ
∂ଶ
w
∂yଶ
+ μ
∂ଶ
w
∂zଶ
4.1.3 Energy Equation
This equation demonstrates that, per unit volume, the change in energy of the fluid moving through a
control volume is equal to the rate of heat transferred into the control volume plus the rate of work
done by surface forces plus the rate of work done by gravity
∂
∂t
൬ρe +
1
2
ρvଶ
൰ +
∂
∂x
൬ρue +
1
2
ρuvଶ
൰ +
∂
∂y
൬ρve +
1
2
ρvvଶ
൰ +
∂
∂z
൬ρwe +
1
2
ρwvଶ
൰ =
k ቆ
∂ଶ
T
∂xଶ
+
∂ଶ
T
∂yଶ
+
∂ଶ
T
∂xzଶቇ − ൬u
∂p
∂x
+ v
∂p
∂y
+ w
∂p
∂z
൰ +
μ ቈu
∂ଶ
u
∂xଶ
+
∂
∂x
൬v
∂v
∂x
+ w
∂w
∂x
൰ + v
∂ଶ
u
∂yଶ
+
∂
∂y
൬u
∂u
∂y
+ w
∂w
∂y
൰ + w
∂ଶ
u
∂zଶ
+
∂
∂z
൬u
∂u
∂z
+ v
∂v
∂z
൰቉
+2μ ቈ
∂ଶ
u
∂xଶ
+
∂u
∂y
∂v
∂x
+
∂ଶ
v
∂yଶ
+
∂v
∂z
∂w
∂y
+
∂ଶ
w
∂zଶ
+
∂w
∂x
∂u
∂z
቉ + ρug୶ + ρvg୷ + ρwg୸
BOUNDARY CONDITIONS
In this simulation Pressure inlet boundary conditions are used to define the fluid pressure at flow
inlets, along with all other scalar properties of the flow. They are suitable for both incompressible and
compressible flow calculations. Pressure inlet boundary conditions can be used when the inlet
pressure is known but the flow rate and/or velocity is not known.
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
Figure.5.
VALIDATION
The problem is solved using ANSYS FLUENT
paper [1], it is found that it gives good agreement with the experimental results of research paper
as shown in following graphs.
Fig.6.1 Comparison of predicted and experimental results for valve lift 10mm performed in
Fig 6.2.1 Prediction of velocity in z=
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
VOLUME 2, ISSUE 9, SEP.
Figure.5. 1 Pressure inlet boundary conditions windows
oblem is solved using ANSYS FLUENT and the code is validated with the results of a
gives good agreement with the experimental results of research paper
as shown in following graphs.
Comparison of predicted and experimental results for valve lift 10mm performed in
previous study
1 Prediction of velocity in z=-15mm for valve lift 10mm in present study
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
5 | P a g e
Pressure inlet boundary conditions windows
the code is validated with the results of a research
gives good agreement with the experimental results of research paper [1]
Comparison of predicted and experimental results for valve lift 10mm performed in
in present study
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
Fig.6.2.2 Prediction of velocity in z=
Fig.6.2.3 Prediction of velocity in z=
It may see from the figures results obtained from the FLUENT shows good agreement with previous
study except in the critical region of valve.
Animated results of FLUENT
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
VOLUME 2, ISSUE 9, SEP.
Prediction of velocity in z=-30mm for valve lift 10mm in present study
Prediction of velocity in z=-45mm for valve lift 10mm in present study
from the figures results obtained from the FLUENT shows good agreement with previous
critical region of valve.
Animated results of FLUENT for 10mm valve lift obtained in present study
Velocity profile for 10mm valve lift
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
6 | P a g e
in present study
in present study
from the figures results obtained from the FLUENT shows good agreement with previous
for 10mm valve lift obtained in present study
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
7 | P a g e
Velocity profile for 10mm valve lift
Velocity streamline for 10mm valve lift
Turbulent kinetic energy profile for 10mm valve lift
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
8 | P a g e
Pressure profile for 10mm valve lift
Velocity contour profile for 10mm valve lift
CONCLUSIONS
To make combustion to happen air flow inside intake port plays a vital role. To get good engine
efficiency with lower emission we need to study the flow inside the intake port, manifold through the
valve. In this thesis we understand the flow characteristics through port inside the engine with the
help of CFD tool FLUENT.
CFD helps to understand the flow field inside the cylinder and also gives depth knowledge of flow in
graphical mode where measurements are not easy to make.
1. Three-dimensional modeling of intake manifold, port and valve are key factors to predict the velocity
contours inside the engine cylinder. From this thesis we can conclude that valve lift affect the flow
except region near the port bend upstream.
2. As the valve lift increases flow separation becomes critical because as valve lift increases losses near
the valve increases.
NOVATEUR PUBLICATIONS
INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT]
ISSN: 2394-3696
VOLUME 2, ISSUE 9, SEP.-2015
9 | P a g e
3. The results obtained from prediction shows good agreement with the experimental results except
some critical region near the valve.
REFERENCES
1. Chen, A., Lee, K.C., Yianneskis, M., and Ganti, G., Velocity Charac- teristics of Steady Flow
Through a Straight Generic Inlet Port, Interna- tional Journal for Numerical Methods in Fluids,
21:571,590, 1995
2. Robert S. Laramee , Daniel Weiskopf , Jürgen Schneider , Avl Graz , Helwig Hauser, Investigating
Swirl and Tumble Flow with a Comparison of Visualization Techniques, In Proceedings IEEE
Visualization, 2004.
3. S. L. V. Prasad, V. Pandurangadu, V. V. Prathibha bharathi and V. V. Naga deepthi, Experimental
study of the effect of air swirl in Intake manifold on diesel engine performance
4. N.Kumar.et.al "Studies on variable swirl intake system for DI diesel engine using CFD", ISSN 0973-
4562 volume 2, number 3 (2007)
5. Soonseong Hong, Byungkeunoh and Yongtae Kim, "Optimization of intake manifold design using
design for six sigma, SAE, 2007-01-3534
6. Mike Dong, Grant Chen, Min Xu and Chao Daniels, “P

Mais conteúdo relacionado

Mais procurados

The KQA April Open Quiz - Finals
The KQA April Open Quiz - FinalsThe KQA April Open Quiz - Finals
The KQA April Open Quiz - Finals
Chandrakant Nair
 

Mais procurados (20)

Mela Quiz Prelims - IIM Ahmedabad Chaos 2020 - by Quiz Cetera
Mela Quiz Prelims - IIM Ahmedabad Chaos 2020 - by Quiz CeteraMela Quiz Prelims - IIM Ahmedabad Chaos 2020 - by Quiz Cetera
Mela Quiz Prelims - IIM Ahmedabad Chaos 2020 - by Quiz Cetera
 
LSD Quiz - NSIT QUIZ FEST 2016
LSD Quiz - NSIT QUIZ FEST 2016LSD Quiz - NSIT QUIZ FEST 2016
LSD Quiz - NSIT QUIZ FEST 2016
 
Rebound- The General Quiz Finals
Rebound- The General Quiz FinalsRebound- The General Quiz Finals
Rebound- The General Quiz Finals
 
Quiz Rathri Finals
Quiz Rathri FinalsQuiz Rathri Finals
Quiz Rathri Finals
 
M.E.L.A. Quiz
M.E.L.A. QuizM.E.L.A. Quiz
M.E.L.A. Quiz
 
Inter Branch Quiz 2023 - Qualifiers
Inter Branch Quiz 2023 - QualifiersInter Branch Quiz 2023 - Qualifiers
Inter Branch Quiz 2023 - Qualifiers
 
Open MELA Quiz Prelims: CQD Fundraiser Quizzes for Assam
Open MELA Quiz Prelims: CQD Fundraiser Quizzes for AssamOpen MELA Quiz Prelims: CQD Fundraiser Quizzes for Assam
Open MELA Quiz Prelims: CQD Fundraiser Quizzes for Assam
 
The KQA April Open Quiz - Finals
The KQA April Open Quiz - FinalsThe KQA April Open Quiz - Finals
The KQA April Open Quiz - Finals
 
The Freshest- A Welcoming Quiz
The Freshest- A Welcoming QuizThe Freshest- A Welcoming Quiz
The Freshest- A Welcoming Quiz
 
MELA Quiz - Prelims | Thomso 17 | IIT Roorkee
MELA Quiz - Prelims | Thomso 17 | IIT RoorkeeMELA Quiz - Prelims | Thomso 17 | IIT Roorkee
MELA Quiz - Prelims | Thomso 17 | IIT Roorkee
 
General Quiz - 2022
General Quiz - 2022General Quiz - 2022
General Quiz - 2022
 
Bollywood Quiz 2017 | Finals
Bollywood Quiz 2017 | FinalsBollywood Quiz 2017 | Finals
Bollywood Quiz 2017 | Finals
 
Genember - A General Quiz in September
Genember - A General Quiz in SeptemberGenember - A General Quiz in September
Genember - A General Quiz in September
 
The Fandom Quiz Prelims by Qilluminati
The Fandom Quiz Prelims by QilluminatiThe Fandom Quiz Prelims by Qilluminati
The Fandom Quiz Prelims by Qilluminati
 
Prelims, MELA Quiz 2017, MIT, Manipal
Prelims, MELA Quiz 2017, MIT, ManipalPrelims, MELA Quiz 2017, MIT, Manipal
Prelims, MELA Quiz 2017, MIT, Manipal
 
The MELA Quiz - DoMS, IIT Roorkee
The MELA Quiz - DoMS, IIT RoorkeeThe MELA Quiz - DoMS, IIT Roorkee
The MELA Quiz - DoMS, IIT Roorkee
 
Melange - French quiz finals - 2015. Put Funda.
Melange - French quiz finals - 2015. Put Funda.Melange - French quiz finals - 2015. Put Funda.
Melange - French quiz finals - 2015. Put Funda.
 
Grand Quizzing Week 2021 | Bollywood Quiz | Prelims
Grand Quizzing Week 2021 | Bollywood Quiz | PrelimsGrand Quizzing Week 2021 | Bollywood Quiz | Prelims
Grand Quizzing Week 2021 | Bollywood Quiz | Prelims
 
IIT(BHU) Dirty Quiz-Prelims
IIT(BHU) Dirty Quiz-PrelimsIIT(BHU) Dirty Quiz-Prelims
IIT(BHU) Dirty Quiz-Prelims
 
General Quiz 5.2.2022
General Quiz 5.2.2022General Quiz 5.2.2022
General Quiz 5.2.2022
 

Semelhante a PORT FLOW SIMULATION OF AN IC ENGINE

CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDERCFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
AM Publications
 
Head Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip BucketsHead Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip Buckets
theijes
 
Prediction of flow characteristics through a circular port of a spool valve u...
Prediction of flow characteristics through a circular port of a spool valve u...Prediction of flow characteristics through a circular port of a spool valve u...
Prediction of flow characteristics through a circular port of a spool valve u...
eSAT Journals
 
Air flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake portAir flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake port
TunAnh309
 
Cfd analysis of rae 2822 supercritical airfoil at transonic mach speeds
Cfd analysis of rae 2822 supercritical airfoil at transonic mach speedsCfd analysis of rae 2822 supercritical airfoil at transonic mach speeds
Cfd analysis of rae 2822 supercritical airfoil at transonic mach speeds
eSAT Journals
 

Semelhante a PORT FLOW SIMULATION OF AN IC ENGINE (20)

CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDERCFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
 
IRJET- Experimental Study on Flow through Venturimeter
IRJET- Experimental Study on Flow through VenturimeterIRJET- Experimental Study on Flow through Venturimeter
IRJET- Experimental Study on Flow through Venturimeter
 
Cfd analysis in an ejector of gas turbine engine test bed
Cfd analysis in an ejector of gas turbine engine test bedCfd analysis in an ejector of gas turbine engine test bed
Cfd analysis in an ejector of gas turbine engine test bed
 
Head Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip BucketsHead Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip Buckets
 
IRJET-Helical Screw-Tape Influence on Swirl Flow Profile in a Diffuser.
IRJET-Helical Screw-Tape Influence on Swirl Flow Profile in a Diffuser.IRJET-Helical Screw-Tape Influence on Swirl Flow Profile in a Diffuser.
IRJET-Helical Screw-Tape Influence on Swirl Flow Profile in a Diffuser.
 
ANALYSIS AND EVALUATION OF COEFFICIENT OF DISCHARGE ON ORIFICE PLATE AND FLOW...
ANALYSIS AND EVALUATION OF COEFFICIENT OF DISCHARGE ON ORIFICE PLATE AND FLOW...ANALYSIS AND EVALUATION OF COEFFICIENT OF DISCHARGE ON ORIFICE PLATE AND FLOW...
ANALYSIS AND EVALUATION OF COEFFICIENT OF DISCHARGE ON ORIFICE PLATE AND FLOW...
 
CFD ANALYSIS IN AN EJECTOR OF GAS TURBINE ENGINE TEST BED
CFD ANALYSIS IN AN EJECTOR OF GAS TURBINE ENGINE TEST BEDCFD ANALYSIS IN AN EJECTOR OF GAS TURBINE ENGINE TEST BED
CFD ANALYSIS IN AN EJECTOR OF GAS TURBINE ENGINE TEST BED
 
DIFFUSER ANGLE CONTROL TO AVOID FLOW SEPARATION
DIFFUSER ANGLE CONTROL TO AVOID FLOW SEPARATIONDIFFUSER ANGLE CONTROL TO AVOID FLOW SEPARATION
DIFFUSER ANGLE CONTROL TO AVOID FLOW SEPARATION
 
Prediction of flow characteristics through a
Prediction of flow characteristics through aPrediction of flow characteristics through a
Prediction of flow characteristics through a
 
Prediction of flow characteristics through a circular port of a spool valve u...
Prediction of flow characteristics through a circular port of a spool valve u...Prediction of flow characteristics through a circular port of a spool valve u...
Prediction of flow characteristics through a circular port of a spool valve u...
 
IRJET- A Literature Review on Investigation of Design Parameter of Cyclone Se...
IRJET- A Literature Review on Investigation of Design Parameter of Cyclone Se...IRJET- A Literature Review on Investigation of Design Parameter of Cyclone Se...
IRJET- A Literature Review on Investigation of Design Parameter of Cyclone Se...
 
J030101053059
J030101053059J030101053059
J030101053059
 
IRJET- A Research Paper on Analysis of De-Laval Nozzle on Ansys Workbench
IRJET-  	  A Research Paper on Analysis of De-Laval Nozzle on Ansys WorkbenchIRJET-  	  A Research Paper on Analysis of De-Laval Nozzle on Ansys Workbench
IRJET- A Research Paper on Analysis of De-Laval Nozzle on Ansys Workbench
 
Air flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake portAir flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake port
 
Cfd analysis of rae 2822 supercritical airfoil at transonic mach speeds
Cfd analysis of rae 2822 supercritical airfoil at transonic mach speedsCfd analysis of rae 2822 supercritical airfoil at transonic mach speeds
Cfd analysis of rae 2822 supercritical airfoil at transonic mach speeds
 
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
 
Experimental Investigations and Computational Analysis on Subsonic Wind Tunnel
Experimental Investigations and Computational Analysis on Subsonic Wind TunnelExperimental Investigations and Computational Analysis on Subsonic Wind Tunnel
Experimental Investigations and Computational Analysis on Subsonic Wind Tunnel
 
The effect of rotational speed variation on the velocity vectors in the singl...
The effect of rotational speed variation on the velocity vectors in the singl...The effect of rotational speed variation on the velocity vectors in the singl...
The effect of rotational speed variation on the velocity vectors in the singl...
 
Numerical Investigation of Turbulent Flow over a Rotating Circular Cylinder u...
Numerical Investigation of Turbulent Flow over a Rotating Circular Cylinder u...Numerical Investigation of Turbulent Flow over a Rotating Circular Cylinder u...
Numerical Investigation of Turbulent Flow over a Rotating Circular Cylinder u...
 
208_CFD
208_CFD208_CFD
208_CFD
 

Mais de ijiert bestjournal

STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR
STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR
STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR
ijiert bestjournal
 
IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW
IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW
IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW
ijiert bestjournal
 

Mais de ijiert bestjournal (20)

CRACKS IN STEEL CASTING FOR VOLUTE CASING OF A PUMP
 CRACKS IN STEEL CASTING FOR VOLUTE CASING OF A PUMP CRACKS IN STEEL CASTING FOR VOLUTE CASING OF A PUMP
CRACKS IN STEEL CASTING FOR VOLUTE CASING OF A PUMP
 
A COMPARATIVE STUDY OF DESIGN OF SIMPLE SPUR GEAR TRAIN AND HELICAL GEAR TRAI...
A COMPARATIVE STUDY OF DESIGN OF SIMPLE SPUR GEAR TRAIN AND HELICAL GEAR TRAI...A COMPARATIVE STUDY OF DESIGN OF SIMPLE SPUR GEAR TRAIN AND HELICAL GEAR TRAI...
A COMPARATIVE STUDY OF DESIGN OF SIMPLE SPUR GEAR TRAIN AND HELICAL GEAR TRAI...
 
COMPARATIVE ANALYSIS OF CONVENTIONAL LEAF SPRING AND COMPOSITE LEAF
COMPARATIVE ANALYSIS OF CONVENTIONAL LEAF SPRING AND COMPOSITE LEAFCOMPARATIVE ANALYSIS OF CONVENTIONAL LEAF SPRING AND COMPOSITE LEAF
COMPARATIVE ANALYSIS OF CONVENTIONAL LEAF SPRING AND COMPOSITE LEAF
 
POWER GENERATION BY DIFFUSER AUGMENTED WIND TURBINE
 POWER GENERATION BY DIFFUSER AUGMENTED WIND TURBINE POWER GENERATION BY DIFFUSER AUGMENTED WIND TURBINE
POWER GENERATION BY DIFFUSER AUGMENTED WIND TURBINE
 
FINITE ELEMENT ANALYSIS OF CONNECTING ROD OF MG-ALLOY
FINITE ELEMENT ANALYSIS OF CONNECTING ROD OF MG-ALLOY FINITE ELEMENT ANALYSIS OF CONNECTING ROD OF MG-ALLOY
FINITE ELEMENT ANALYSIS OF CONNECTING ROD OF MG-ALLOY
 
REVIEW ON CRITICAL SPEED IMPROVEMENT IN SINGLE CYLINDER ENGINE VALVE TRAIN
REVIEW ON CRITICAL SPEED IMPROVEMENT IN SINGLE CYLINDER ENGINE VALVE TRAINREVIEW ON CRITICAL SPEED IMPROVEMENT IN SINGLE CYLINDER ENGINE VALVE TRAIN
REVIEW ON CRITICAL SPEED IMPROVEMENT IN SINGLE CYLINDER ENGINE VALVE TRAIN
 
ENERGY CONVERSION PHENOMENON IN IMPLEMENTATION OF WATER LIFTING BY USING PEND...
ENERGY CONVERSION PHENOMENON IN IMPLEMENTATION OF WATER LIFTING BY USING PEND...ENERGY CONVERSION PHENOMENON IN IMPLEMENTATION OF WATER LIFTING BY USING PEND...
ENERGY CONVERSION PHENOMENON IN IMPLEMENTATION OF WATER LIFTING BY USING PEND...
 
SCUDERI SPLIT CYCLE ENGINE: REVOLUTIONARY TECHNOLOGY & EVOLUTIONARY DESIGN RE...
SCUDERI SPLIT CYCLE ENGINE: REVOLUTIONARY TECHNOLOGY & EVOLUTIONARY DESIGN RE...SCUDERI SPLIT CYCLE ENGINE: REVOLUTIONARY TECHNOLOGY & EVOLUTIONARY DESIGN RE...
SCUDERI SPLIT CYCLE ENGINE: REVOLUTIONARY TECHNOLOGY & EVOLUTIONARY DESIGN RE...
 
EXPERIMENTAL EVALUATION OF TEMPERATURE DISTRIBUTION IN JOURNAL BEARING OPERAT...
EXPERIMENTAL EVALUATION OF TEMPERATURE DISTRIBUTION IN JOURNAL BEARING OPERAT...EXPERIMENTAL EVALUATION OF TEMPERATURE DISTRIBUTION IN JOURNAL BEARING OPERAT...
EXPERIMENTAL EVALUATION OF TEMPERATURE DISTRIBUTION IN JOURNAL BEARING OPERAT...
 
STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR
STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR
STUDY OF SOLAR THERMAL CAVITY RECEIVER FOR PARABOLIC CONCENTRATING COLLECTOR
 
DESIGN, OPTIMIZATION AND FINITE ELEMENT ANALYSIS OF CRANKSHAFT
DESIGN, OPTIMIZATION AND FINITE ELEMENT ANALYSIS OF CRANKSHAFTDESIGN, OPTIMIZATION AND FINITE ELEMENT ANALYSIS OF CRANKSHAFT
DESIGN, OPTIMIZATION AND FINITE ELEMENT ANALYSIS OF CRANKSHAFT
 
ELECTRO CHEMICAL MACHINING AND ELECTRICAL DISCHARGE MACHINING PROCESSES MICRO...
ELECTRO CHEMICAL MACHINING AND ELECTRICAL DISCHARGE MACHINING PROCESSES MICRO...ELECTRO CHEMICAL MACHINING AND ELECTRICAL DISCHARGE MACHINING PROCESSES MICRO...
ELECTRO CHEMICAL MACHINING AND ELECTRICAL DISCHARGE MACHINING PROCESSES MICRO...
 
HEAT TRANSFER ENHANCEMENT BY USING NANOFLUID JET IMPINGEMENT
HEAT TRANSFER ENHANCEMENT BY USING NANOFLUID JET IMPINGEMENTHEAT TRANSFER ENHANCEMENT BY USING NANOFLUID JET IMPINGEMENT
HEAT TRANSFER ENHANCEMENT BY USING NANOFLUID JET IMPINGEMENT
 
MODIFICATION AND OPTIMIZATION IN STEEL SANDWICH PANELS USING ANSYS WORKBENCH
MODIFICATION AND OPTIMIZATION IN STEEL SANDWICH PANELS USING ANSYS WORKBENCH MODIFICATION AND OPTIMIZATION IN STEEL SANDWICH PANELS USING ANSYS WORKBENCH
MODIFICATION AND OPTIMIZATION IN STEEL SANDWICH PANELS USING ANSYS WORKBENCH
 
IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW
IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW
IMPACT ANALYSIS OF ALUMINUM HONEYCOMB SANDWICH PANEL BUMPER BEAM: A REVIEW
 
DESIGN OF WELDING FIXTURES AND POSITIONERS
DESIGN OF WELDING FIXTURES AND POSITIONERSDESIGN OF WELDING FIXTURES AND POSITIONERS
DESIGN OF WELDING FIXTURES AND POSITIONERS
 
ADVANCED TRANSIENT THERMAL AND STRUCTURAL ANALYSIS OF DISC BRAKE BY USING ANS...
ADVANCED TRANSIENT THERMAL AND STRUCTURAL ANALYSIS OF DISC BRAKE BY USING ANS...ADVANCED TRANSIENT THERMAL AND STRUCTURAL ANALYSIS OF DISC BRAKE BY USING ANS...
ADVANCED TRANSIENT THERMAL AND STRUCTURAL ANALYSIS OF DISC BRAKE BY USING ANS...
 
REVIEW ON MECHANICAL PROPERTIES OF NON-ASBESTOS COMPOSITE MATERIAL USED IN BR...
REVIEW ON MECHANICAL PROPERTIES OF NON-ASBESTOS COMPOSITE MATERIAL USED IN BR...REVIEW ON MECHANICAL PROPERTIES OF NON-ASBESTOS COMPOSITE MATERIAL USED IN BR...
REVIEW ON MECHANICAL PROPERTIES OF NON-ASBESTOS COMPOSITE MATERIAL USED IN BR...
 
PERFORMANCE EVALUATION OF TRIBOLOGICAL PROPERTIES OF COTTON SEED OIL FOR MULT...
PERFORMANCE EVALUATION OF TRIBOLOGICAL PROPERTIES OF COTTON SEED OIL FOR MULT...PERFORMANCE EVALUATION OF TRIBOLOGICAL PROPERTIES OF COTTON SEED OIL FOR MULT...
PERFORMANCE EVALUATION OF TRIBOLOGICAL PROPERTIES OF COTTON SEED OIL FOR MULT...
 
MAGNETIC ABRASIVE FINISHING
MAGNETIC ABRASIVE FINISHINGMAGNETIC ABRASIVE FINISHING
MAGNETIC ABRASIVE FINISHING
 

Último

Call Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort Service
Call Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort ServiceCall Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort Service
Call Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort Service
9953056974 Low Rate Call Girls In Saket, Delhi NCR
 
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
ssuser89054b
 
VIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 Booking
VIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 BookingVIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 Booking
VIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 Booking
dharasingh5698
 
FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756
FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756
FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756
dollysharma2066
 

Último (20)

Call Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort Service
Call Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort ServiceCall Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort Service
Call Girls in Netaji Nagar, Delhi 💯 Call Us 🔝9953056974 🔝 Escort Service
 
CCS335 _ Neural Networks and Deep Learning Laboratory_Lab Complete Record
CCS335 _ Neural Networks and Deep Learning Laboratory_Lab Complete RecordCCS335 _ Neural Networks and Deep Learning Laboratory_Lab Complete Record
CCS335 _ Neural Networks and Deep Learning Laboratory_Lab Complete Record
 
NFPA 5000 2024 standard .
NFPA 5000 2024 standard                                  .NFPA 5000 2024 standard                                  .
NFPA 5000 2024 standard .
 
KubeKraft presentation @CloudNativeHooghly
KubeKraft presentation @CloudNativeHooghlyKubeKraft presentation @CloudNativeHooghly
KubeKraft presentation @CloudNativeHooghly
 
VIP Model Call Girls Kothrud ( Pune ) Call ON 8005736733 Starting From 5K to ...
VIP Model Call Girls Kothrud ( Pune ) Call ON 8005736733 Starting From 5K to ...VIP Model Call Girls Kothrud ( Pune ) Call ON 8005736733 Starting From 5K to ...
VIP Model Call Girls Kothrud ( Pune ) Call ON 8005736733 Starting From 5K to ...
 
Thermal Engineering -unit - III & IV.ppt
Thermal Engineering -unit - III & IV.pptThermal Engineering -unit - III & IV.ppt
Thermal Engineering -unit - III & IV.ppt
 
Double rodded leveling 1 pdf activity 01
Double rodded leveling 1 pdf activity 01Double rodded leveling 1 pdf activity 01
Double rodded leveling 1 pdf activity 01
 
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
 
VIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 Booking
VIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 BookingVIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 Booking
VIP Call Girls Ankleshwar 7001035870 Whatsapp Number, 24/07 Booking
 
UNIT - IV - Air Compressors and its Performance
UNIT - IV - Air Compressors and its PerformanceUNIT - IV - Air Compressors and its Performance
UNIT - IV - Air Compressors and its Performance
 
FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756
FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756
FULL ENJOY Call Girls In Mahipalpur Delhi Contact Us 8377877756
 
Water Industry Process Automation & Control Monthly - April 2024
Water Industry Process Automation & Control Monthly - April 2024Water Industry Process Automation & Control Monthly - April 2024
Water Industry Process Automation & Control Monthly - April 2024
 
ONLINE FOOD ORDER SYSTEM PROJECT REPORT.pdf
ONLINE FOOD ORDER SYSTEM PROJECT REPORT.pdfONLINE FOOD ORDER SYSTEM PROJECT REPORT.pdf
ONLINE FOOD ORDER SYSTEM PROJECT REPORT.pdf
 
Top Rated Pune Call Girls Budhwar Peth ⟟ 6297143586 ⟟ Call Me For Genuine Se...
Top Rated  Pune Call Girls Budhwar Peth ⟟ 6297143586 ⟟ Call Me For Genuine Se...Top Rated  Pune Call Girls Budhwar Peth ⟟ 6297143586 ⟟ Call Me For Genuine Se...
Top Rated Pune Call Girls Budhwar Peth ⟟ 6297143586 ⟟ Call Me For Genuine Se...
 
data_management_and _data_science_cheat_sheet.pdf
data_management_and _data_science_cheat_sheet.pdfdata_management_and _data_science_cheat_sheet.pdf
data_management_and _data_science_cheat_sheet.pdf
 
(INDIRA) Call Girl Meerut Call Now 8617697112 Meerut Escorts 24x7
(INDIRA) Call Girl Meerut Call Now 8617697112 Meerut Escorts 24x7(INDIRA) Call Girl Meerut Call Now 8617697112 Meerut Escorts 24x7
(INDIRA) Call Girl Meerut Call Now 8617697112 Meerut Escorts 24x7
 
Intro To Electric Vehicles PDF Notes.pdf
Intro To Electric Vehicles PDF Notes.pdfIntro To Electric Vehicles PDF Notes.pdf
Intro To Electric Vehicles PDF Notes.pdf
 
Call Girls Pimpri Chinchwad Call Me 7737669865 Budget Friendly No Advance Boo...
Call Girls Pimpri Chinchwad Call Me 7737669865 Budget Friendly No Advance Boo...Call Girls Pimpri Chinchwad Call Me 7737669865 Budget Friendly No Advance Boo...
Call Girls Pimpri Chinchwad Call Me 7737669865 Budget Friendly No Advance Boo...
 
Call Girls Walvekar Nagar Call Me 7737669865 Budget Friendly No Advance Booking
Call Girls Walvekar Nagar Call Me 7737669865 Budget Friendly No Advance BookingCall Girls Walvekar Nagar Call Me 7737669865 Budget Friendly No Advance Booking
Call Girls Walvekar Nagar Call Me 7737669865 Budget Friendly No Advance Booking
 
Thermal Engineering-R & A / C - unit - V
Thermal Engineering-R & A / C - unit - VThermal Engineering-R & A / C - unit - V
Thermal Engineering-R & A / C - unit - V
 

PORT FLOW SIMULATION OF AN IC ENGINE

  • 1. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 1 | P a g e PORT FLOW SIMULATION OF AN IC ENGINE Himanth Kumar H Y, PG Student Department of Mechanical Engineering, Vidyavardhaka College of Engineering, Mysuru, India Jayashankar N Associate professor, Mechanical department, Vidyavardhaka College of Engineering, Mysuru, India ABSTRACT This paper deals with the numerical analysis of 3d model which has inlet port diameter 46mm, valve diameter 43mm and the length and diameter of the cylinder is 562mm and 93.65mm respectively which is developed to study the effect of valve lift on the flow of fluid inside the cylinder. For different valve lifts velocity will change inside the cylinder. Results of CFD simulation indicated that valve lift affects velocity flow field inside the cylinder. It also proved that CFD is a convenient tool for designing and optimizing the flow field in the engine. KEYWORDS-Computational fluid dynamics; intake manifold; inlet port; Numerical simulation; INTRODUCTION The internal combustion engine usually consists of four cycles such as intake, compression, expansion (including combustion) and exhaust. Out of these four processes intake and compression strokes are most important as these strokes influences the pattern of air flow coming inside cylinder during intake stroke and it generates the condition needed for the fuel injection during compression stroke. For maximizing the air passing into the cylinder manifold design has to be optimized. Hence design of intake manifold is more important in engine design. Experimental methods would cost time and money to achieve this. Using CFD tool without undergoing any time consuming experiment engine efficiency can be estimated. Short discussions of the previous studies of authors are presented here. Chen et.al [1] gives result of fluid flow through an IC engine inlet port both in experimental and computational mode. The port was straight generic inlet port. They used CFD tool to analyze the velocity contours near port region. They have used LDA and LSFV technique to analyze fluid flow. Both experimental and prediction results shows that the valve lift that affect the flow Robert et.al [2] studied the two common motions in an automobile engine they are tumble and swirl motion using visualization techniques. Benny et.al [3] investigates the effect of helical, spiral manifold configuration on air motion in a diesel engine. Using CFD tool flow patterns of these different manifold configurations are studied. The CFD results of swirl velocity inside combustion chamber are compared with experimental results.
  • 2. INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] Prasad.et.al [4] investigates the swirl air created due to injecting air into the manifold. To direct air flow into the inlet manifold they have grooved the inlet manifold with helical groove to create turbulence in the manifold. The tests are conducted by va maintained constant. The main objective of this proje intake manifold, inlet port and valve enhances the performance of the engine by improving combustion rate II MATHEMATICAL FORMULATION 2.1 The physical model and coordinate system A 3D model of a inlet port and valve with cylinder is s (Ver. 14.5). Table 2.1 Dimension Diameter of Diameter of the valve Diameter of the cylinder Length of the Valve lift Fig 2.1 Theoretical model MESHING The model is created using ANSYS FLUENT In-cylinder problems solved in Fluent consist of three stages geometry into different zones and mesh them properly. The second stage is to set up the engine case inside Fluent with the help of a setup journal. The third stage is to perform a transient in INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] VOLUME 2, ISSUE 9, SEP. sad.et.al [4] investigates the swirl air created due to injecting air into the manifold. To direct air flow into the inlet manifold they have grooved the inlet manifold with helical groove to create turbulence in the manifold. The tests are conducted by varying dimensions of groove and speed was The main objective of this project is to analyze the velocity characteristics of fluid flow through the intake manifold, inlet port and valve to get optimized swirl and tumble motion, so that one can enhances the performance of the engine by improving combustion rate. II MATHEMATICAL FORMULATION 2.1 The physical model and coordinate system inlet port and valve with cylinder is shown in fig is created in Table 2.1 Dimensions of various parts of model as shown in Fig 2.1 inlet and outlet port 46 & 39.5 mm iameter of the valve 43 mm ameter of the cylinder 93.65 mm Length of the cylinder 562 mm Valve lift 10 mm Theoretical model Geometry model created in fluent model is created using ANSYS FLUENT software. solved in Fluent consist of three stages. The first stage is to decompose the geometry into different zones and mesh them properly. The second stage is to set up the engine case inside Fluent with the help of a setup journal. The third stage is to perform a transient in-cylinder simulation. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 2 | P a g e sad.et.al [4] investigates the swirl air created due to injecting air into the manifold. To direct air flow into the inlet manifold they have grooved the inlet manifold with helical groove to create rying dimensions of groove and speed was ct is to analyze the velocity characteristics of fluid flow through the to get optimized swirl and tumble motion, so that one can is created in ANSYS FLUENT shown in Fig 2.1 & 39.5 mm 93.65 mm 562 mm Geometry model created in fluent first stage is to decompose the The second stage is to set up the engine case inside Fluent with the help of a setup journal.
  • 3. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 3 | P a g e First, the surface is meshed with triangular element. In order to resolve the turbulent boundary layer on the solid surfaces, it is best to have growing prismatic cells from the Valve surfaces. Finally the remaining region in the domain is filled with tetrahedral cells. No of elements is used for mesh generation is 11 to 12 lakhs approximately. The domain has been subdivided into growing boxes to make it easier to generate the grid. The choice for the elements has been both tetrahedral and hexahedral mesh volumes. Fig 3.1 Meshed model in FLUENT GOVERNING EQUATIONS There are mainly three equations we solve in computational fluid dynamics problem. They are Continuity equation, Momentum equation (Navier Stokes equation) and Energy equation. 4.1.1 Continuity Equation A continuity equation expresses a conservation law by “Equating a net flux over a surface with a loss or gain of material within the surface”. Continuity equations often can be expressed in either integral or differential form as shown below. 0= ∂ ∂ + ∫∫ cvcs dA t dAV ρρ This is a statement of the principle of mass conservation for a steady, one-dimensional flow, with one inlet and one outlet. ( ) 0= ∂ ∂ +∇ t V ρ ρ
  • 4. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 4 | P a g e Where, ^^^ k z j y i x ∂ ∂ + ∂ ∂ + ∂ ∂ =∇ ∂ρ ∂t + ∂(ρ. u) ∂x + ∂(ρ. v) ∂y + ∂(ρ. w) ∂z = 0 4.1.2 Momentum (Navier Stokes) Equations The momentum equation is a statement of Newton's Second Law and relates the sum of the forces acting on an element of fluid to its acceleration or rate of change of momentum. The Newton’s second law of motion F = ma forms the basis of the momentum equation. ρ ∂u ∂t + ρu ∂u ∂x + ρv ∂u ∂y + ρw ∂u ∂z = ρg୶ − ∂p ∂x + μ ∂ଶ u ∂xଶ + μ ∂ଶ u ∂yଶ + μ ∂ଶ u ∂zଶ ρ ∂v ∂t + ρu ∂v ∂x + ρv ∂v ∂y + ρw ∂v ∂z = ρg୷ − ∂p ∂y + μ ∂ଶ v ∂xଶ + μ ∂ଶ v ∂yଶ + μ ∂ଶ v ∂zଶ ρ ∂w ∂t + ρu ∂w ∂x + ρv ∂w ∂y + ρw ∂w ∂z = ρg୸ − ∂p ∂z + μ ∂ଶ w ∂xଶ + μ ∂ଶ w ∂yଶ + μ ∂ଶ w ∂zଶ 4.1.3 Energy Equation This equation demonstrates that, per unit volume, the change in energy of the fluid moving through a control volume is equal to the rate of heat transferred into the control volume plus the rate of work done by surface forces plus the rate of work done by gravity ∂ ∂t ൬ρe + 1 2 ρvଶ ൰ + ∂ ∂x ൬ρue + 1 2 ρuvଶ ൰ + ∂ ∂y ൬ρve + 1 2 ρvvଶ ൰ + ∂ ∂z ൬ρwe + 1 2 ρwvଶ ൰ = k ቆ ∂ଶ T ∂xଶ + ∂ଶ T ∂yଶ + ∂ଶ T ∂xzଶቇ − ൬u ∂p ∂x + v ∂p ∂y + w ∂p ∂z ൰ + μ ቈu ∂ଶ u ∂xଶ + ∂ ∂x ൬v ∂v ∂x + w ∂w ∂x ൰ + v ∂ଶ u ∂yଶ + ∂ ∂y ൬u ∂u ∂y + w ∂w ∂y ൰ + w ∂ଶ u ∂zଶ + ∂ ∂z ൬u ∂u ∂z + v ∂v ∂z ൰቉ +2μ ቈ ∂ଶ u ∂xଶ + ∂u ∂y ∂v ∂x + ∂ଶ v ∂yଶ + ∂v ∂z ∂w ∂y + ∂ଶ w ∂zଶ + ∂w ∂x ∂u ∂z ቉ + ρug୶ + ρvg୷ + ρwg୸ BOUNDARY CONDITIONS In this simulation Pressure inlet boundary conditions are used to define the fluid pressure at flow inlets, along with all other scalar properties of the flow. They are suitable for both incompressible and compressible flow calculations. Pressure inlet boundary conditions can be used when the inlet pressure is known but the flow rate and/or velocity is not known.
  • 5. INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] Figure.5. VALIDATION The problem is solved using ANSYS FLUENT paper [1], it is found that it gives good agreement with the experimental results of research paper as shown in following graphs. Fig.6.1 Comparison of predicted and experimental results for valve lift 10mm performed in Fig 6.2.1 Prediction of velocity in z= INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] VOLUME 2, ISSUE 9, SEP. Figure.5. 1 Pressure inlet boundary conditions windows oblem is solved using ANSYS FLUENT and the code is validated with the results of a gives good agreement with the experimental results of research paper as shown in following graphs. Comparison of predicted and experimental results for valve lift 10mm performed in previous study 1 Prediction of velocity in z=-15mm for valve lift 10mm in present study NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 5 | P a g e Pressure inlet boundary conditions windows the code is validated with the results of a research gives good agreement with the experimental results of research paper [1] Comparison of predicted and experimental results for valve lift 10mm performed in in present study
  • 6. INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] Fig.6.2.2 Prediction of velocity in z= Fig.6.2.3 Prediction of velocity in z= It may see from the figures results obtained from the FLUENT shows good agreement with previous study except in the critical region of valve. Animated results of FLUENT INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] VOLUME 2, ISSUE 9, SEP. Prediction of velocity in z=-30mm for valve lift 10mm in present study Prediction of velocity in z=-45mm for valve lift 10mm in present study from the figures results obtained from the FLUENT shows good agreement with previous critical region of valve. Animated results of FLUENT for 10mm valve lift obtained in present study Velocity profile for 10mm valve lift NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 6 | P a g e in present study in present study from the figures results obtained from the FLUENT shows good agreement with previous for 10mm valve lift obtained in present study
  • 7. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 7 | P a g e Velocity profile for 10mm valve lift Velocity streamline for 10mm valve lift Turbulent kinetic energy profile for 10mm valve lift
  • 8. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 8 | P a g e Pressure profile for 10mm valve lift Velocity contour profile for 10mm valve lift CONCLUSIONS To make combustion to happen air flow inside intake port plays a vital role. To get good engine efficiency with lower emission we need to study the flow inside the intake port, manifold through the valve. In this thesis we understand the flow characteristics through port inside the engine with the help of CFD tool FLUENT. CFD helps to understand the flow field inside the cylinder and also gives depth knowledge of flow in graphical mode where measurements are not easy to make. 1. Three-dimensional modeling of intake manifold, port and valve are key factors to predict the velocity contours inside the engine cylinder. From this thesis we can conclude that valve lift affect the flow except region near the port bend upstream. 2. As the valve lift increases flow separation becomes critical because as valve lift increases losses near the valve increases.
  • 9. NOVATEUR PUBLICATIONS INTERNATIONAL JOURNAL OF INNOVATIONS IN ENGINEERING RESEARCH AND TECHNOLOGY [IJIERT] ISSN: 2394-3696 VOLUME 2, ISSUE 9, SEP.-2015 9 | P a g e 3. The results obtained from prediction shows good agreement with the experimental results except some critical region near the valve. REFERENCES 1. Chen, A., Lee, K.C., Yianneskis, M., and Ganti, G., Velocity Charac- teristics of Steady Flow Through a Straight Generic Inlet Port, Interna- tional Journal for Numerical Methods in Fluids, 21:571,590, 1995 2. Robert S. Laramee , Daniel Weiskopf , Jürgen Schneider , Avl Graz , Helwig Hauser, Investigating Swirl and Tumble Flow with a Comparison of Visualization Techniques, In Proceedings IEEE Visualization, 2004. 3. S. L. V. Prasad, V. Pandurangadu, V. V. Prathibha bharathi and V. V. Naga deepthi, Experimental study of the effect of air swirl in Intake manifold on diesel engine performance 4. N.Kumar.et.al "Studies on variable swirl intake system for DI diesel engine using CFD", ISSN 0973- 4562 volume 2, number 3 (2007) 5. Soonseong Hong, Byungkeunoh and Yongtae Kim, "Optimization of intake manifold design using design for six sigma, SAE, 2007-01-3534 6. Mike Dong, Grant Chen, Min Xu and Chao Daniels, “P