Title of article
Formulation of an RP-1 pyrolysis surrogate from shock tube measurements of fuel and ethylene time histories
Author/Authors
MacDonald، نويسنده , , Megan E. and Davidson، نويسنده , , David F. and Hanson، نويسنده , , Ronald K. and Pitz، نويسنده , , William J. and Mehl، نويسنده , , Marcos and Westbrook، نويسنده , , Charles K.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2013
Pages
9
From page
1051
To page
1059
Abstract
RP-1 and ethylene time histories have been measured during RP-1 pyrolysis, allowing determination of ethylene yields and overall fuel decomposition rates for RP-1 near 20 atm and between 1050 K and 1500 K. A decomposition surrogate for RP-1 was formulated using the components n-dodecane, methylcyclohexane, and iso-cetane by targeting three decomposition characteristics of the fuel: compound class, overall fuel decomposition rate, and ethylene yield. Decomposition of this surrogate mixture was modeled using a newly developed detailed mechanism and the simulations are compared to the experimentally measured RP-1 and ethylene time histories. Comparisons between modeled and measured ethylene yields and overall fuel decomposition rates are also reported.
Keywords
Rocket propellant RP-1 , laser absorption , Pyrolysis , Shock tubes , Ethylene time-histories
Journal title
Fuel
Serial Year
2013
Journal title
Fuel
Record number
1468708
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