Three-dimensional standing oblique detonation wave in a hypersonic flow
Author:
Affiliation:
1. Nagoya University, Japan
2. Mitsubishi Heavy Industries, Ltd., Nagoya, Japan
3. National Aerospace Laboratory, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-478
Reference9 articles.
1. Induced Combustion with Oblique Shocks: Comparison of Experiment and Kinetic Calculations. AlAA J. V01.l. pp.2778-278411963).
2. Gea 1er:StudiesinConnection with Stabilized Gaseous Detonation Waves. 7th Symposium on Combustion, pp.766-772,1958.
3. Numerical Analysis of Two-Dimensional Nonsteady Detonations
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