Velocimetry Measurements of Unstart of an Inlet-Isolator Model in Mach 5 Flow
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
2. Istanbul Technical University, 34469 Istanbul, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050037
Reference42 articles.
1. Fluid Phenomena in Scramjet Combustion Systems
2. AIAA Education Series;Heiser W. H.,1993
3. Pressure Distribution Measurements in Scramjet Isolators under Asymmetric Supersonic Flow
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