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SI engine combustion - MIT

SI engine combustion - MIT

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Schematic of SI engine flame propagation Fig. 9-4 Schematic of flame propagation in SI engine: unburned gas (U) to left of flame, burned gas to right. A denotes adiabatic burned-gas core, BL denotes thermal boundary layer in burned gas. Heat transfer Work transfer 5 Typical pressure and mass fraction burned (xb) curves 0 200 400 600 0 5 10 15 20 25

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