1997
DOI: 10.1080/00102209708935637
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Gas Dynamic Features of Self Ignition of Non Diluted Fuel/Air Mixtures at High Pressure

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Cited by 7 publications
(9 citation statements)
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“…Historically, transient shock ignition phenomena have been utilized to generate conditions to study the ignition and combustion of homogenous premixed mixtures of gaseous fuels and oxidizers. Extensive literature exists on single pulse and reflected shock tube studies of premixed hydrogen-oxygen, methaneoxygen, and natural gas-oxygen mixtures (e.g., Eubank et al, 1981;Blumenthal et al, 1996;Huang et al, 2004). As noted earlier, much less work has addressed transient shock phenomena produced by compressed gas releases into air as a potential spontaneous ignition source.…”
Section: Simple Transient Shock Theory and Implicationsmentioning
confidence: 99%
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“…Historically, transient shock ignition phenomena have been utilized to generate conditions to study the ignition and combustion of homogenous premixed mixtures of gaseous fuels and oxidizers. Extensive literature exists on single pulse and reflected shock tube studies of premixed hydrogen-oxygen, methaneoxygen, and natural gas-oxygen mixtures (e.g., Eubank et al, 1981;Blumenthal et al, 1996;Huang et al, 2004). As noted earlier, much less work has addressed transient shock phenomena produced by compressed gas releases into air as a potential spontaneous ignition source.…”
Section: Simple Transient Shock Theory and Implicationsmentioning
confidence: 99%
“…The calculations shown in Figure 8a were performed using a constant volume assumption with the chemical ignition delay time determined as the time to pressure rise. This is a common approach for calculating shock tube ignition delay times for premixed gas mixtures (Blumenthal et al, 1996). A constant pressure assumption and other criteria for defining ignition delay yield times of very similar magnitude.…”
Section: Simple Transient Shock Theory and Implicationsmentioning
confidence: 99%
“…The shock tube data obtained by (Snyder, Robertson et al 1965;Bhaskaran, Gupta et al 1973;Slack 1977;Blumenthal, Fieweger et al 1996;Wang, Olivier et al 2003), also exhibit an activation energy transition as a function of pressure and temperature. Quantitatively, the shock tube data and simulation are in agreement in the high-temperature (17 kcal/mol activation energy) region.…”
Section: Autoignitionmentioning
confidence: 99%
“…iv | P a g e Figure 19: Effect of initial mixture temperature on flashback and blow off velocity gradients for propane-air flames in tubes (Dugger 1955 Peschke and Spadaccini (1985) and Santoro et al (2009), and the Shock Tube Results of Snyder et al (1965), Blumenthal et al (1996), Slack (1977), and Wang (2003) …”
Section: Uci Combustion Laboratorymentioning
confidence: 99%
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