Multiple shock-shock interference on a cylindrical leading edge
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11181
Reference14 articles.
1. Survey of viscous interactions associated with high Mach number flight
2. Flow-thermal-structural study of aerodynamically heated leading edges
3. Experimental shock-wave interference heating on a cylinder at Mach 6and 8
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