Experimental Investigation of the Shock Train in an Isolator of a Scramjet Inlet
Author:
Affiliation:
1. Shock Wave Laboratory, RWTH Aachen University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2220
Reference13 articles.
1. Experimental Investigation of the Internal Flow Field of a Scramjet Engine
2. Numerical Investigation of the Isolator Flow Field of a SCRAMJET Engine with Elevated Wall Temperatures
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