Computation of unsteady shock-induced combustion using logarithmic species conservation equations
Author:
Affiliation:
1. Eloret Institute, Palo Alto, California 94303
2. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11667
Reference17 articles.
1. Studies of hypervelocity firings into mixtures of hydrogen with air or with oxygen
2. Onset of oscillation in the presence of detonation wave weakening
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