2010
DOI: 10.1016/j.energy.2010.04.003
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Second-law analyses applied to a spark ignition engine under surrogate fuels for gasoline

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Cited by 15 publications
(7 citation statements)
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“…The thermal mechanism dominates in high temperature combustion over a fairly wide range of equivalence ratios, while the Fennimore mechanism is important in rich combustion. For the features of the system and high temperature chamber combustion the NO x formation was modeled using the Zeldovich mechanism [4,10]. This mechanism consists of three reversible chain reactions: As the mole balance is applied during combustion cycle we have a closed system, and only the term of reaction and accumulation are take into account.…”
Section: Chemical Kinetic Modelmentioning
confidence: 99%
“…The thermal mechanism dominates in high temperature combustion over a fairly wide range of equivalence ratios, while the Fennimore mechanism is important in rich combustion. For the features of the system and high temperature chamber combustion the NO x formation was modeled using the Zeldovich mechanism [4,10]. This mechanism consists of three reversible chain reactions: As the mole balance is applied during combustion cycle we have a closed system, and only the term of reaction and accumulation are take into account.…”
Section: Chemical Kinetic Modelmentioning
confidence: 99%
“…where θ is the crank angle, θ0 is the angle where the start of combustion occurs, θ is the total combustion duration and α and m are adjustable parameters. Actual mass fraction burned curves was fitted with α = 4.6 and m = 2 [16]. The mass fraction that remains unburned is given by (1 − x b ).…”
Section: Combustion Burn Rate Sub-modelmentioning
confidence: 99%
“…Here K u and K b are the heat transfer coefficients for burned and unburned zone and depend of the Reynolds number and the thermal conductivity of each zone. h R is the radiation transfer coefficient, A u and A b are the areas of each zone and T w is the transfer wall temperature which is taken as 420 K [16].The heat transfer for compression and expansion could be calculated with an easier expression…”
Section: Heat Transfer Sub-modelmentioning
confidence: 99%
“…The thermo-mechanical availability can be determined using the following formula [17]: The thermo-mechanical availability can be determined using the following formula [17]:…”
Section: Model Descriptionmentioning
confidence: 99%