Investigation of kinetics of iso-octane ignition under scramjet conditions

Autor:	Shehan A. P. Corera, Skip Williams, Sukh Sidhu, Moshan S. P. Kahandawala, Campbell D. Carter
Rok vydání:	2006
Předmět:	Atmospheric pressure Chemistry Organic Chemistry Thermodynamics Atmospheric temperature range Biochemistry law.invention Shock (mechanics) Inorganic Chemistry Ignition system Minimum ignition energy law Deflagration Scramjet Physics::Chemical Physics Physical and Theoretical Chemistry Shock tube
Zdroj:	International Journal of Chemical Kinetics. 38:194-201
ISSN:	1097-4601 0538-8066
DOI:	10.1002/kin.20155
Popis:	A single pulse reflected shock tube was used to investigate iso-octane ignition over the temperature range of 900-1400 K at a pressure of 1 atm. To account for the anticipated long ignition delay times at the lower temperatures, long shock tube dwell times (12 ms) at lower temperature and near atmospheric pressure were achieved by using argon-helium mix as a driver gas. Chemical thermometer experiments were conducted to remove any uncertainties in determining post-reflected shock temperatures. The ignition delay data obtained in this study are in good agreement (in the overlap region) with the iso-octane ignition data from a previous shock tube study. However, the activation energy of iso-octane ignition obtained in this study in the lower temperature region (
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::ea7ef62f5f6a5cf2118a11f8e27a3c9c https://doi.org/10.1002/kin.20155 Zobrazit plný text záznamu Plný text ve formátu PDF Plný text ve formátu HTML
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