A three-dimensional model for spark ignition engines: Initial validation
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Summary
A three-dimensional model for the cold flow motion and/or combustion of a homogeneous charge in Spark Ignition Engines was developed. An explicit predictor-corrector technique was employed. The model was validated in its two-dimensional version by comparing the computed TDC turbulence intensity with a parametric set of experimental data and with the results obtained with a different, previously validated, two-dimensional model. The fully three-dimensional model was then tested to simulate the cold flow motion of a homogeneous charge in a pancake-like chamber. It was concluded that the model can be used for cold flow simulation of Spark Ignition Engine.
Keywords
Experimental Data Combustion Mechanical Engineer Civil Engineer Turbulence IntensityList of symbols
- A
Preexponential factor, mole1/2/cm1.5−s
- b
Boundary velocity, cm/s
- B
Bore, cm
- CFL
Courant-Friedrichs-Lewy number
- \(C_{ \in _1 } ,C_{ \in _2 } ,C_{ \in _3 } ,\)
Constants in the turbulence model
- cp
Coefficient of specific heat at constantp, erg/g −K
- cν
Coefficient of specific heat at constant volume erg/g −K
- CL
Clearance, cm
- CR
Compression ratio
- D
Diffusivity, cm2/s
- EA
Activation energy, erg/mol
- F
Fuel
- I
Inert
- I
Specific internal energy, erg/g
- İ
Specific internal energy release, erg/g − s
- Jk
Mass flux of speciesk, g/cm2 − s
- Jq
Energy flux, erg/g − cm2 − s
- h
Specific enthalpy, erg/g
- k
Kinetic energy of turbulence, cm2/s2
- n
Unit normal to the wall surface
- O
Oxidizer
- p
Pressure, dynes/cm2
- P
Product
- Pr
Prandtl number
- R
Universal gas constant, erg/mole −K
- RPM
Engine speed, min−1
- t
Time, sec
- t
Unit tangent
- T
Temperature,K
- u
Component of velocity inx-direction, cm/s
- \(\underline{\underline U} ,\underline{\underline U}\)
Unit tensor
- v
Component of velocity iny-direction, cm/s
- vp
Mean piston speed, cm/s
- V
Control volume, cm3
- ∂V
Control volume, cm2
- x, y, z
Coordinate directions
- w
Component of velocity inz-direction, cm/s
- W
Molecular weight, g/mole
- Yk
Mass fraction of kth species
Greek Symbols
- α, β
Constants for determining initial values ofk and∈
- γ
Ratio of specific heat coefficients
- δ
Piston displacement
- Δx, Δy, Δz
Mesh spacing inx, y, z, cm
- ∈
Dissipation rate of turbulence kinetic energy, cm2/s3
- ηv
Volumetric efficiency
- κ
Von Karman's constant
- λ
Heat conductivity, erg/g − cm − s −K
- μ
Viscosity, g/cm − s
- ν
Kinematic viscosity, cm2/s
- ν′, ν″
Stoichimetric coefficients
- \(\dot \omega\)
Reaction rate g/cm3 − s
- ρ
Density, g/cm3
- \(\underline{\underline \sigma }\)
Stress tensor, dynes/cm2
- σ
Prandtl number
- Φ
Scalar variable
- θ
Crank angle, deg
Superscripts
- F
Fuel
- k
k − th species
- n
Time leveln
- \(n{\mathbf{ }}\widetilde + {\mathbf{ }}1\)
Predicted time level
- n+1
Corrected time level
- O
Oxygen
- T
Transpose
- ′
Fluctuating component
- *
Non-dimensional quantities
Subscripts
- BCD
Bottom Dead Center
- F
Fuel
- INIT
Initial
- LAM
Laminar
- O2, O
Oxygen
- P
Products
- TDC
Top Dead Center
- TURB
Turbulent
- w
Wall
Sommario
E' stato sviluppato un modello tridimensionale, per studiare la fluidodinamica con o senza combustione di una carica omogenea in un Motore ad Accensione Comandata. E' stata impiegata una tecnica esplicita del tipo predictor-corrector. Il modello è stato convalidato nella sua versïone bidimensionale confrontando la intensità della turbolenza calcolata al punto morto superiore con dati sperimentali e con risultati ottenuti con un diverso modello bidimensionale precedentemente convalidato. Il modello tridimensionale è stato quindi usato per simulare la fluidodinamica fredda di una carica omogenea in una camera di combustione di tipo pancake. Si è concluso che il modello può essere impiegato per la simulazione della fluidodinamica in un Motore ad Accencione Comandata.
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