This is a steady-cycle educational model. Changing a control solves a new cycle. RPM is prescribed; the simulation does not solve crank acceleration, mechanical loading, friction, knock, fluid flow, or chemical kinetics. The 3D assembly is illustrative, not manufacturing CAD.
- Gas & mixture
- Ideal gas, γ = 1.35, air/fuel = 14.7
- Fuel heat
- 44 MJ/kg × 0.93 efficiency
- Temperatures
- Inlet 310 K · wall 450 K
- Wall heat transfer
- 130 W/(m² K), assumed constant
- Intake / exhaust
- (0.30 + 0.70 × throttle) bar / 1.06 bar
- Valve timing
- Ideal boundaries at dead centers; no overlap
- Burn fraction
- xb = (1 − exp(−6.9u³)) / (1 − exp(−6.9)), u ∈ [0,1]
- Burn duration
- 55° + RPM × 0.002°
- Firing order
- 1 · 8 · 4 · 3 · 6 · 5 · 7 · 2, one event every 90°
- Acoustics
- Pulse resonators; no exhaust-pipe fluid solver or recording
Background: NASA cycle thermodynamics · Work done by a gas