Unsteady characteristics of a hypersonic type IV shock interaction
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46876
Reference22 articles.
1. 'Bowcutt, K. G. "Optimization of Hypersonic Waveriders Derived from Cone Flows-Including Viscous Effects," Ph.D. Dissertation,Univ. of Maryland, College Park, MD, 1986.
2. Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow
3. Computational studies of a fluid spike as a leading edge protection device for shock-shock interference heating
4. Shock interference studies on a circular cylinder at Mach 16
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