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Investigation of the flow field
in a single-cylinder Spark Ignition
engine using OpenFOAM
Antonio D’Andrea
M.Sc. Mechanical Engineering
Politecnico di Milano
Examiner: Prof. Michael Oevermann
Combustion and Propulsion system
Chalmers University of Technology
8/27/2019 Chalmers 2
Overview
• Introduction
• Modeling framework
• Stl Generation
• Mesh Generation
• Mesh motion strategy
• Optical research engine and
Simulation settings overview
• Results
• In-cylinder pressure
• Velocity profiles (Quantitative Analysis)
• Flow visualization (Qualitative Analysis)
• Conclusion
Objectives
Overall fluid-dynamic
domain
• Full-cycle 3D simulation
 Main objective is to capture the
correct in-cylinder turbulence.
• To Investigate
 In-Cylinder Pressure
Velocity field
8/27/2019 Chalmers 3
Modeling Framework - Stl Generation
stl files:
• Cylinder Head
• SparkPlug
• Injector
• Piston
• Liner
• Intake Valves (Bottom, Top, Stem)
• Exhaust Valves (Bottom, Top, Stem)
• Inlet cross-section
• Outlet cross-section
• Exhaust Manifold
• Intake Manifold
8/27/2019 Chalmers 4
Stl Foundation File
Modeling Framework - Stl Generation
• Engine Stl generation file:
 Automatic procedure adopting shell script
 5 crank angle degree step interval (full-cycle → 144 cases)
8/27/2019 Chalmers 5
Modeling Framework – Mesh Generation
• BlockMesh
• SnappyHexMesh
8/27/2019 Chalmers 6
Modeling Framework - Mesh motion strategy
• OpenFOAM dynamicFvMesh model.
• Grid motion based on displacement Laplacian Equation:
 Keeps track of grid points positions;
 Calculates grid point velocities;
 Updates grid points positions;
 Mesh deformation dealt with mapping (“mapFielDict”)
8/27/2019 Chalmers 7
Modeling Framework - Research engine overview
• TU-Darmstadt optical research Engine
Spray-Guided head geometry
8/27/2019 Chalmers 8
Modeling Framework – Simulation settings
• Numerical Set-up overview:
 OpenFOAM 2.2.2;
 LES simulation;
 Solver based on sonicEngineFoam;
 Pressure-based compressible solver;
 Unstructured hex grids;
 Mesh motion without topological changes;
 Mapping and solution in parallel;
 Backward implicit time integration;
8/27/2019 Chalmers 9
 Time varying pressure boundary conditions;
• Three preliminary consecutive Cycles with
fixed mesh:
 2.4 - 6.5 million cells (TDC – BDC) ducts
included;
Cycle 4
8/27/2019 Chalmers 10
Results
8/27/2019 Chalmers 11
Results – In-cylinder pressure
60 CAD bTDC 30 CAD bTDC
15 CAD bTDC TDC
Sampling line at z = 5mm
8/27/2019 12
Results – Quantitative Analysis
Sampling line position z=5mm
z
xy
Reference U magnitude field
cycle2
8/27/2019 Chalmers 13
Ux[m/s]Uz[m/s]
X axis [mm] X axis [mm] X axis [mm] X axis [mm]
Sampling line at z = 0mm
60 CAD bTDC 30 CAD bTDC
15 CAD bTDC TDC
8/27/2019 14
Results – Quantitative Analysis
z
xy
Sampling line position z=0mm
Reference U magnitude field
cycle2
8/27/2019 Chalmers 15
Results – Quantitative Analysis
Ux[m/s]Uz[m/s]
X axis [mm] X axis [mm] X axis [mm] X axis [mm]
Sampling line at z = -10mm
60 CAD bTDC 45 CAD bTDC
15 CAD bTDC TDC
8/27/2019 16
Results – Quantitative Analysis
z
xy
Sampling line position z=-10mm
Reference U magnitude field
cycle2
8/27/2019 Chalmers 17
Results – Quantitative Analysis
Ux[m/s]Uz[m/s]
X axis [mm] X axis [mm]
Results – Flow visualization
• Tumble plane PIV
Measurements
Numerical
8/27/2019 Chalmers 19
Results – Qualitative Analysis
CYCLE 1 CYCLE 2PIV
300bTDC250bTDC
CYCLE 3
z
xy
8/27/2019 Chalmers 20
Results – Qualitative Analysis
180bTDC CYCLE 1 CYCLE 2PIV CYCLE 3130bTDC
z
xy
CYCLE 1 CYCLE 2PIV
50bTDC30bTDC
z
xy
8/27/2019 Chalmers 21
Results – Qualitative Analysis
CYCLE 1 CYCLE 2PIV CYCLE 3
PIV
U[m/s]
X direction
zdirection
8/27/2019 Chalmers 22
Results – Qualitative Analysis
• Qualitative analysis for center of tumble motion at 250°bTDC (Max valve Lift).
CYCLE 4
Conclusion - Future work
8/27/2019 Chalmers 23
• Multi-cycles simulations:
 more motored cycles to improve results
towards TDC;
• Implementation of combustion model:
 Fired engine simulations in stratified condition.
 Spray direct injection simulation within engine
model;
T
Conclusion – Preliminary Fired case
8/27/2019 Chalmers 24
• Implementation of Weller
combustion model:
 Fired engine simulation
with premixed fuel.
8/27/2019 Chalmers 25
Thank you for
your attention
Chalmers Presentation: Flow Field In A Single-Cylinder Spark Ignition Engine Using OPENFOAM
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Ad

Chalmers Presentation: Flow Field In A Single-Cylinder Spark Ignition Engine Using OPENFOAM

  • 1. Investigation of the flow field in a single-cylinder Spark Ignition engine using OpenFOAM Antonio D’Andrea M.Sc. Mechanical Engineering Politecnico di Milano Examiner: Prof. Michael Oevermann Combustion and Propulsion system Chalmers University of Technology
  • 2. 8/27/2019 Chalmers 2 Overview • Introduction • Modeling framework • Stl Generation • Mesh Generation • Mesh motion strategy • Optical research engine and Simulation settings overview • Results • In-cylinder pressure • Velocity profiles (Quantitative Analysis) • Flow visualization (Qualitative Analysis) • Conclusion
  • 3. Objectives Overall fluid-dynamic domain • Full-cycle 3D simulation  Main objective is to capture the correct in-cylinder turbulence. • To Investigate  In-Cylinder Pressure Velocity field 8/27/2019 Chalmers 3
  • 4. Modeling Framework - Stl Generation stl files: • Cylinder Head • SparkPlug • Injector • Piston • Liner • Intake Valves (Bottom, Top, Stem) • Exhaust Valves (Bottom, Top, Stem) • Inlet cross-section • Outlet cross-section • Exhaust Manifold • Intake Manifold 8/27/2019 Chalmers 4
  • 5. Stl Foundation File Modeling Framework - Stl Generation • Engine Stl generation file:  Automatic procedure adopting shell script  5 crank angle degree step interval (full-cycle → 144 cases) 8/27/2019 Chalmers 5
  • 6. Modeling Framework – Mesh Generation • BlockMesh • SnappyHexMesh 8/27/2019 Chalmers 6
  • 7. Modeling Framework - Mesh motion strategy • OpenFOAM dynamicFvMesh model. • Grid motion based on displacement Laplacian Equation:  Keeps track of grid points positions;  Calculates grid point velocities;  Updates grid points positions;  Mesh deformation dealt with mapping (“mapFielDict”) 8/27/2019 Chalmers 7
  • 8. Modeling Framework - Research engine overview • TU-Darmstadt optical research Engine Spray-Guided head geometry 8/27/2019 Chalmers 8
  • 9. Modeling Framework – Simulation settings • Numerical Set-up overview:  OpenFOAM 2.2.2;  LES simulation;  Solver based on sonicEngineFoam;  Pressure-based compressible solver;  Unstructured hex grids;  Mesh motion without topological changes;  Mapping and solution in parallel;  Backward implicit time integration; 8/27/2019 Chalmers 9  Time varying pressure boundary conditions; • Three preliminary consecutive Cycles with fixed mesh:  2.4 - 6.5 million cells (TDC – BDC) ducts included;
  • 11. 8/27/2019 Chalmers 11 Results – In-cylinder pressure
  • 12. 60 CAD bTDC 30 CAD bTDC 15 CAD bTDC TDC Sampling line at z = 5mm 8/27/2019 12 Results – Quantitative Analysis Sampling line position z=5mm z xy Reference U magnitude field cycle2
  • 13. 8/27/2019 Chalmers 13 Ux[m/s]Uz[m/s] X axis [mm] X axis [mm] X axis [mm] X axis [mm]
  • 14. Sampling line at z = 0mm 60 CAD bTDC 30 CAD bTDC 15 CAD bTDC TDC 8/27/2019 14 Results – Quantitative Analysis z xy Sampling line position z=0mm Reference U magnitude field cycle2
  • 15. 8/27/2019 Chalmers 15 Results – Quantitative Analysis Ux[m/s]Uz[m/s] X axis [mm] X axis [mm] X axis [mm] X axis [mm]
  • 16. Sampling line at z = -10mm 60 CAD bTDC 45 CAD bTDC 15 CAD bTDC TDC 8/27/2019 16 Results – Quantitative Analysis z xy Sampling line position z=-10mm Reference U magnitude field cycle2
  • 17. 8/27/2019 Chalmers 17 Results – Quantitative Analysis Ux[m/s]Uz[m/s] X axis [mm] X axis [mm]
  • 18. Results – Flow visualization • Tumble plane PIV Measurements Numerical
  • 19. 8/27/2019 Chalmers 19 Results – Qualitative Analysis CYCLE 1 CYCLE 2PIV 300bTDC250bTDC CYCLE 3 z xy
  • 20. 8/27/2019 Chalmers 20 Results – Qualitative Analysis 180bTDC CYCLE 1 CYCLE 2PIV CYCLE 3130bTDC z xy
  • 21. CYCLE 1 CYCLE 2PIV 50bTDC30bTDC z xy 8/27/2019 Chalmers 21 Results – Qualitative Analysis CYCLE 1 CYCLE 2PIV CYCLE 3
  • 22. PIV U[m/s] X direction zdirection 8/27/2019 Chalmers 22 Results – Qualitative Analysis • Qualitative analysis for center of tumble motion at 250°bTDC (Max valve Lift). CYCLE 4
  • 23. Conclusion - Future work 8/27/2019 Chalmers 23 • Multi-cycles simulations:  more motored cycles to improve results towards TDC; • Implementation of combustion model:  Fired engine simulations in stratified condition.  Spray direct injection simulation within engine model;
  • 24. T Conclusion – Preliminary Fired case 8/27/2019 Chalmers 24 • Implementation of Weller combustion model:  Fired engine simulation with premixed fuel.
  • 25. 8/27/2019 Chalmers 25 Thank you for your attention
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