2009
DOI: 10.1016/j.combustflame.2009.08.003
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Influence of autoignition delay time characteristics of different fuels on pressure waves and knock in reciprocating engines

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Cited by 175 publications
(95 citation statements)
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“…1. In the very early stages of knock, originating at a single hot spot, the amplitude of the pressure pulse is proportional to 2   [38]. The low values of   r T E   ln -tend to confirm that combustion was in the auto-ignitive mode.…”
Section: Engine Performance and The Detonation Peninsulamentioning
confidence: 96%
See 1 more Smart Citation
“…1. In the very early stages of knock, originating at a single hot spot, the amplitude of the pressure pulse is proportional to 2   [38]. The low values of   r T E   ln -tend to confirm that combustion was in the auto-ignitive mode.…”
Section: Engine Performance and The Detonation Peninsulamentioning
confidence: 96%
“…Conditions F, G, I, and J represent super-knock, associated with auto-ignitive pre-ignition [38], and subsequent strong developing detonations.…”
Section: Engine Performance and The Detonation Peninsulamentioning
confidence: 99%
“…80 It is interesting to note that up to 2011, no LES studies on engine knock were published at all, as pointed out by Rutland. 14 Since then, some initial attempts to model engine knock using LES have been reported. [84][85][86] Although significant improvements have been achieved in describing the fluid flow, mixture formation and the combustion process leading to end-gas auto-ignition, knock prediction was still only qualitative since auto-ignition is only a necessary but not a sufficient criterion for knock, as pointed out in a series of articles by Bradley et al, 87 Gu et al, 88 Bradley and Kalghatgi 89 and Kalghatgi and Bradley. 90 The first promising works to predict engine knock were published only recently.…”
Section: Knock and Abnormal Combustionmentioning
confidence: 99%
“…Data points indicated by are from a rapid compression machine, in which maximum knock pressure amplitudes varied as  -1.923 , close to the estimate of  -2 in [26]. The diverse operational conditions show that entry into the detonation peninsula is associated with the onset of knock, which can become severe (1) arise partly from the greater charge cooling that arises in modern engines, and partly from the smaller inverse exponent for, non-PRF, realistic fuels [1,3], that determines the effect of pressure on i  .…”
Section:   / Diagram For Different Enginesmentioning
confidence: 99%