Interaction between detonation waves and flowfields.
Author:
Affiliation:
1. Air Force Institute of Technology (Air University), Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4093
Reference9 articles.
1. Shock-induced combustion with oblique shocks- comparison of experiment and kinetic calculations
2. Reviewer's Comment
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