Dissertation/Thesis Abstract

Numerical simulation of liquid oxygen and liquid methane glow plug ignition system
by Iizuka, Toshiaki, M.S., California State University, Long Beach, 2011, 88; 1490389
Abstract (Summary)

This thesis investigates the ability of numerical simulations to analyze the ignition process of liquid oxygen (LOX) / liquid methane (LCt4). Experimental data from a NASA glow plug ignition system is used for validation. The ignition process is simulated numerically by solving the Reynolds Averaged Navier-Stokes (RANS) equations with combustion.

Successful ignition requires sufficient enthalpy and adequate equivalence ratio. The calculated region of equivalence ratio required to achieve successful ignition is identified and compared with experimental data. Numerical predictions agree with experimental data between a ratio of 0.31 and 0.42. At higher equivalence ratios, some disagreements exist, likely due to differences in geometry between tests and simulations. The numerical results indicate that, for the simulated configuration, successful ignition is achieved in the 0.31 and 0.90 equivalence ratio range.

Indexing (document details)
Advisor: Besnard, Eric
Commitee:
School: California State University, Long Beach
School Location: United States -- California
Source: MAI 49/04M, Masters Abstracts International
Source Type: DISSERTATION
Subjects: Aerospace engineering
Keywords:
Publication Number: 1490389
ISBN: 9781124550022
Copyright © 2019 ProQuest LLC. All rights reserved. Terms and Conditions Privacy Policy Cookie Policy
ProQuest