1994
DOI: 10.1016/s0082-0784(06)80803-9
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Shock-tube investigations on the self-ignition of hydrocarbon-air mixtures at high pressures

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Cited by 85 publications
(57 citation statements)
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“…These data together with the model simulations are depicted in Fig 4. It is clear that, in the temperature range 600 to 675 K, the model simulation predicts more reactivity than observed experimentally, with more O 2 reacted and more CO, CO 2 , and H 2 O produced. We have not been able to gain better agreement as to do so would result in poorer agreement with the shock tube ignition-delay data of Fieweger et al [6,7], discussed below.…”
Section: Princeton Variable Pressure Flow Reactormentioning
confidence: 62%
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“…These data together with the model simulations are depicted in Fig 4. It is clear that, in the temperature range 600 to 675 K, the model simulation predicts more reactivity than observed experimentally, with more O 2 reacted and more CO, CO 2 , and H 2 O produced. We have not been able to gain better agreement as to do so would result in poorer agreement with the shock tube ignition-delay data of Fieweger et al [6,7], discussed below.…”
Section: Princeton Variable Pressure Flow Reactormentioning
confidence: 62%
“…Below, we describe how this mechanism was used to simulate experimental results obtained in an atmospheric pressure flow reactor [20], a variable pressure flow reactor [15,22] at 12.5 atm, and a complementarily different flow reactor [23]. Moreover, results obtained in a jet-stirred reactor [10], shock tubes [5][6][7], and in a motored engine [17] are also simulated. Overall, good agreement is obtained between model and experiment.…”
Section: Mechanism Validationmentioning
confidence: 99%
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