Experimental Investigation of Wall and Total Temperature Influence on a Shock Train
Author:
Affiliation:
1. Shock Wave Laboratory, RWTH Aachen University, 52056 Aachen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052599
Reference25 articles.
1. On the influence of elevated surface temperatures on hypersonic shock wave/boundary layer interaction at a heated ramp model
2. Experimental Investigation of the Internal Flow Field of a Scramjet Engine
3. Numerical Investigation of the Isolator Flow Field of a SCRAMJET Engine with Elevated Wall Temperatures
4. Experimental Investigation of the Shock Train in an Isolator of a Scramjet Inlet
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