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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1331
A Comparative CFD Analysis for Air Swirl on Conventional Valve and
Modified Valve with Skirting of Diesel Engine
Nilesh Kakad1, Prof. S.B. Bawaskar2, Prof. Ratnadip Bhorge3
1Student, Dept. of Mechanical Engineering, SVCET Rajuri, Maharshtra, India
2Faculty, Dept. of Mechanical Engineering, SVCET Rajuri, Maharshtra, India
3Faculty, Dept. of Automobile Engineering, DPCOE Pune, Maharshtra, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - In diesel engines swirl is needed for proper
mixing of fuel and air. Evaluation of design of engine intake
port using virtual bench “CFD” is significantly improved by
identifying best practiceswhichreducesthetimeconsumption.
In DI engines swirl is needed for proper mixing of fuel and air.
Evaluation of design of engine intake port using virtual bench
“CFD” is significantly improved by identifying best practices
which reduces the time consumption. The engine with two
ports is considered which is designed to study air flow motion.
3D model of the flow field were computed to analyze air flow
motion in the considered diesel engine. Calculation was
carried out at different valve lifts to calculate air flow velocity
inside different sections of engine. Two sets of engine
geometries are considered one is with conventional valve and
another is with valve with skirting. The comparative analysis
was done to determine better swirl in cylinder .The analysis
was done to develop standard methodology for future
iteration.
Key Words: Swirl, fluent, Skirting, IC engine.
1. INTRODUCTION
Internal combustion engines are seen every day in
automobiles, trucks, andbuses.Therearebasicallytwotypes
of I.C. ignition engines, those which need a spark plug, and
those that rely on compression of a fluid. Compression
ignition engines take atmospheric airandfuel,compressitto
high pressure and temperature, at which time combustion
occurs. These engines are high in power and fuel economy.
Engines are also divided into four stroke and two stroke
engines. In four stroke engines the piston accomplishes four
distinct strokes for every two revolutions of the crankshaft.
Combustion in diesel engines depends upon the injection
process and fuel jet interaction with the air inside the
cylinder. Knowledge of the air movement insidethecylinder
is of great importance for the improvement of the
combustion process. In DI engines swirl isneededforproper
mixing of fuel and air. Moreover, the efficiency of engine can
be improved by increasing burn rate of fuel/air mixture.
Swirl and fuel motion can have significant effect on fuel air
mixing, combustion, heat transfer, and emissions.
Turbulence inside the cylinder is high during the intake and
then decreases as the flow rate slows near the bottom dead
centre (BDC). It increases again during the compression
stroke as swirl, squish andtumbleincreasenearthetopdead
centre (TDC). The high turbulence near TDC when ignition
occurs is much required for combustion process of the
engine. It breaks up and spreads the flame front many times
faster than that of a laminar flame. Both fuel and air is
consumed in a very short time, whereby self-ignition and
knock are avoided. This turbulence is enhanced by the
expansion of engine cylinder duringthecombustionprocess.
2. PROBLEM DEFINATION
The problems associated with conventional test rig flow
bench are the time and cost consumed by them. Design
engineers should work a lot on the design and construction
of the model and the errors involved in test rig affect the
results.
3. METHODOLOGY
1. Creating geometry using using ANSYS Design
Modeler or import geometry from any of the CAD
Software.
2. Creating fluid body (Flow model)
3. Mesh the model.
4. Selecting material.
5. Defining zones.
6. Importing in ANSYS fluent.
7. Defining boundary conditions.
8. Obtaining result.
4. 3D MODEL
In this project two sets of engines are taken into account. In
one case the swirl motion in conventional valve engine is
done and in another case swirl motion is studied by adding
skirting to the valve. Skirting acts as barrier to the flow and
hence causes more swirling.
Table -1: Valve design specification
Parameter Dimensions(mm)
Base diameter of
valve
26.3
Stem length of valve 67
Diameter of stem 7
Diameter of pipe 27.3
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1332
Fig -1: Engine geometry after assembly
5. ANALYSIS
Flow bench testing does not provide a very efficient path to
the final design because the designers do not have aninsight
on the details of recirculation areas, turbulence and design-
imposed pressure losses. CFD (Virtual Flow Bench), an
analysis tool used to improve the port design by simulating
the flow in alternative port designs.CFDsimulationprovides
fluid velocity and pressure throughout the solution domain
with complex geometries and boundary conditions.
So the analysis is done using ANSYS fluent. In one case the
swirl motion in conventional valve engine is done and in
another case swirl motion is studied by adding skirting to
the valve. Skirting acts as barrier to the flow and hence
causes more swirling. The engine used for simulation is
stationary engine with bore diameter 79.5mm and stroke
length 95.5mm. The RPM of engine used is 2000.
The geometric details of considered engine are given in
Table 2 below
Table -2: Geometrical specifications of engine
Sr. No. Parameters Dimensions
1 Bore 79.5mm
2 Stroke 95.5mm
3 Squish 1mm
4 Engine RPM 2000
5 Intake valve opening 4 degrees ATDC
6 Intake valve closing 25 degrees ABDC
Table -3: Input values for air flow calculations
2 Parameters Value
1 Area at inlet
0.00052209
2 Density
1.225 kg/
3 Mass flow 0.006395603 kg/s
4 Factor 1.5
5 Turbulent intensity 0.05
6 Epsilon turbulent
Dissipation rate
0.09
7 Kinetic energy 0.375
8 Epsilon turbulent
dissipation rate
0.147625498
Giving the above inputs values to ANSYS fluent and post
processing is done.
5. RESULT AND DISCUSSION
Case I: Considering Pressure contour
Fig -2: Pressure contour for conventional valve with
minimum valve lift
By observing the contour in Fig 2 we can find that the
pressure is higher in the pipe side and it reduces when air
enters the cylinder.
Fig -3: Pressure contour for modified valve
By observing the contour fig 3 we can find that the pressure
is higher in the pipe side and it reduces when air enters the
cylinder.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1333
Case II: Considering velocity contour
Fig -4: Velocity contour for conventional valve
By observing the contour in fig 3 we can find that the
velocity is higher near valve side and it reduces when air
enters the cylinder.
Fig -5: Velocity contour for modified valve
By observing the contour fig 5 we can find thatthevelocityis
higher near the valve side and it reduces when air entersthe
cylinder. It is also observed that near the skirting velocity is
slightly increased.
6. CONCLUSIONS
For better combustion of the fuel in engine, air fuel mixing
plays an important role. Velocity of air should be more near
valve for proper mixing of the air and fuel mixture, velocity
of air in liner part is very important. Higher will be the
velocity in that region more turbulence will be created.
Which will lead to better swirl motion. More turbulencealso
ensures better air and fuel mixture.
REFERENCES
[1] Laxmikant P. Narkhede & AtulPatil, Optimization For
Intake Port, International Journal Of Mechanical And
Production Engineering Research And Development
(Ijmperd), 2014
[2] Bassem Ramadan, study of swirl generation in KIVA-
3V, kettering university.
[3] T. Lucchini, G. Montenegro, G. D’Errico CFD
Simulations of I.C. Engines: Combustion, Internal
Flows, integrated 1D-MultiD simulations 2007
[4] Klas Fridolin, Cfd For Air Induction Systems With
Openfoam Chalmers University Of Technology
Gothenburg, Sweden 2012
[5] Jorge Martins, Senhorinha Teixeira, Stijn Coene,
Design Of An Inlet Track Of A Small I. C. Engine For
Swirl Enhancement, 20th International Congress of
Mechanical Engineering, 2009
[6] H.Mohamed Niyaz, Prof. A.S.Dhekane, Design
Optimization Of Intake Port In Diesel Engine By Using
CFD Analysis, International Journal Of Engineering
Research & Technology (IJERT), ISSN: 2278-0181,
Vol. 2 Issue 11, November – 2013
[7] Ervin Adorean, Gheorghe-AlexandruRadu, diesel
engine in-cylinder calculations with openfoam.

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  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1331 A Comparative CFD Analysis for Air Swirl on Conventional Valve and Modified Valve with Skirting of Diesel Engine Nilesh Kakad1, Prof. S.B. Bawaskar2, Prof. Ratnadip Bhorge3 1Student, Dept. of Mechanical Engineering, SVCET Rajuri, Maharshtra, India 2Faculty, Dept. of Mechanical Engineering, SVCET Rajuri, Maharshtra, India 3Faculty, Dept. of Automobile Engineering, DPCOE Pune, Maharshtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - In diesel engines swirl is needed for proper mixing of fuel and air. Evaluation of design of engine intake port using virtual bench “CFD” is significantly improved by identifying best practiceswhichreducesthetimeconsumption. In DI engines swirl is needed for proper mixing of fuel and air. Evaluation of design of engine intake port using virtual bench “CFD” is significantly improved by identifying best practices which reduces the time consumption. The engine with two ports is considered which is designed to study air flow motion. 3D model of the flow field were computed to analyze air flow motion in the considered diesel engine. Calculation was carried out at different valve lifts to calculate air flow velocity inside different sections of engine. Two sets of engine geometries are considered one is with conventional valve and another is with valve with skirting. The comparative analysis was done to determine better swirl in cylinder .The analysis was done to develop standard methodology for future iteration. Key Words: Swirl, fluent, Skirting, IC engine. 1. INTRODUCTION Internal combustion engines are seen every day in automobiles, trucks, andbuses.Therearebasicallytwotypes of I.C. ignition engines, those which need a spark plug, and those that rely on compression of a fluid. Compression ignition engines take atmospheric airandfuel,compressitto high pressure and temperature, at which time combustion occurs. These engines are high in power and fuel economy. Engines are also divided into four stroke and two stroke engines. In four stroke engines the piston accomplishes four distinct strokes for every two revolutions of the crankshaft. Combustion in diesel engines depends upon the injection process and fuel jet interaction with the air inside the cylinder. Knowledge of the air movement insidethecylinder is of great importance for the improvement of the combustion process. In DI engines swirl isneededforproper mixing of fuel and air. Moreover, the efficiency of engine can be improved by increasing burn rate of fuel/air mixture. Swirl and fuel motion can have significant effect on fuel air mixing, combustion, heat transfer, and emissions. Turbulence inside the cylinder is high during the intake and then decreases as the flow rate slows near the bottom dead centre (BDC). It increases again during the compression stroke as swirl, squish andtumbleincreasenearthetopdead centre (TDC). The high turbulence near TDC when ignition occurs is much required for combustion process of the engine. It breaks up and spreads the flame front many times faster than that of a laminar flame. Both fuel and air is consumed in a very short time, whereby self-ignition and knock are avoided. This turbulence is enhanced by the expansion of engine cylinder duringthecombustionprocess. 2. PROBLEM DEFINATION The problems associated with conventional test rig flow bench are the time and cost consumed by them. Design engineers should work a lot on the design and construction of the model and the errors involved in test rig affect the results. 3. METHODOLOGY 1. Creating geometry using using ANSYS Design Modeler or import geometry from any of the CAD Software. 2. Creating fluid body (Flow model) 3. Mesh the model. 4. Selecting material. 5. Defining zones. 6. Importing in ANSYS fluent. 7. Defining boundary conditions. 8. Obtaining result. 4. 3D MODEL In this project two sets of engines are taken into account. In one case the swirl motion in conventional valve engine is done and in another case swirl motion is studied by adding skirting to the valve. Skirting acts as barrier to the flow and hence causes more swirling. Table -1: Valve design specification Parameter Dimensions(mm) Base diameter of valve 26.3 Stem length of valve 67 Diameter of stem 7 Diameter of pipe 27.3
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1332 Fig -1: Engine geometry after assembly 5. ANALYSIS Flow bench testing does not provide a very efficient path to the final design because the designers do not have aninsight on the details of recirculation areas, turbulence and design- imposed pressure losses. CFD (Virtual Flow Bench), an analysis tool used to improve the port design by simulating the flow in alternative port designs.CFDsimulationprovides fluid velocity and pressure throughout the solution domain with complex geometries and boundary conditions. So the analysis is done using ANSYS fluent. In one case the swirl motion in conventional valve engine is done and in another case swirl motion is studied by adding skirting to the valve. Skirting acts as barrier to the flow and hence causes more swirling. The engine used for simulation is stationary engine with bore diameter 79.5mm and stroke length 95.5mm. The RPM of engine used is 2000. The geometric details of considered engine are given in Table 2 below Table -2: Geometrical specifications of engine Sr. No. Parameters Dimensions 1 Bore 79.5mm 2 Stroke 95.5mm 3 Squish 1mm 4 Engine RPM 2000 5 Intake valve opening 4 degrees ATDC 6 Intake valve closing 25 degrees ABDC Table -3: Input values for air flow calculations 2 Parameters Value 1 Area at inlet 0.00052209 2 Density 1.225 kg/ 3 Mass flow 0.006395603 kg/s 4 Factor 1.5 5 Turbulent intensity 0.05 6 Epsilon turbulent Dissipation rate 0.09 7 Kinetic energy 0.375 8 Epsilon turbulent dissipation rate 0.147625498 Giving the above inputs values to ANSYS fluent and post processing is done. 5. RESULT AND DISCUSSION Case I: Considering Pressure contour Fig -2: Pressure contour for conventional valve with minimum valve lift By observing the contour in Fig 2 we can find that the pressure is higher in the pipe side and it reduces when air enters the cylinder. Fig -3: Pressure contour for modified valve By observing the contour fig 3 we can find that the pressure is higher in the pipe side and it reduces when air enters the cylinder.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1333 Case II: Considering velocity contour Fig -4: Velocity contour for conventional valve By observing the contour in fig 3 we can find that the velocity is higher near valve side and it reduces when air enters the cylinder. Fig -5: Velocity contour for modified valve By observing the contour fig 5 we can find thatthevelocityis higher near the valve side and it reduces when air entersthe cylinder. It is also observed that near the skirting velocity is slightly increased. 6. CONCLUSIONS For better combustion of the fuel in engine, air fuel mixing plays an important role. Velocity of air should be more near valve for proper mixing of the air and fuel mixture, velocity of air in liner part is very important. Higher will be the velocity in that region more turbulence will be created. Which will lead to better swirl motion. More turbulencealso ensures better air and fuel mixture. REFERENCES [1] Laxmikant P. Narkhede & AtulPatil, Optimization For Intake Port, International Journal Of Mechanical And Production Engineering Research And Development (Ijmperd), 2014 [2] Bassem Ramadan, study of swirl generation in KIVA- 3V, kettering university. [3] T. Lucchini, G. Montenegro, G. D’Errico CFD Simulations of I.C. Engines: Combustion, Internal Flows, integrated 1D-MultiD simulations 2007 [4] Klas Fridolin, Cfd For Air Induction Systems With Openfoam Chalmers University Of Technology Gothenburg, Sweden 2012 [5] Jorge Martins, Senhorinha Teixeira, Stijn Coene, Design Of An Inlet Track Of A Small I. C. Engine For Swirl Enhancement, 20th International Congress of Mechanical Engineering, 2009 [6] H.Mohamed Niyaz, Prof. A.S.Dhekane, Design Optimization Of Intake Port In Diesel Engine By Using CFD Analysis, International Journal Of Engineering Research & Technology (IJERT), ISSN: 2278-0181, Vol. 2 Issue 11, November – 2013 [7] Ervin Adorean, Gheorghe-AlexandruRadu, diesel engine in-cylinder calculations with openfoam.