Ram-Scram Transition and Flame/Shock-Train Interactions in a Model Scramjet Experiment
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34486
Reference29 articles.
1. Structure of Shock Waves in Cylindrical Ducts
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4. Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts
5. Turbulence phenomena in a multiple normal shock wave/turbulent boundary-layer interaction
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