Approximate solutions for oblique detonations in the hypersonic limit
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana 46556
2. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10978
Reference29 articles.
1. Morphology of a standing oblique detonation wave
2. Some properties of stationary detonation waves
3. Propagation of Weak Disturbances in a Gas Subject to Relaxation Effects
4. The linearized flow of a dissociating gas
5. Some Aspects of Nonequilibrium Flows
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