Investigation of Unsteady Edney Type IV and VII Shock–Shock Interactions
Author:
Affiliation:
1. 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.J054298
Reference31 articles.
1. SandersonS. “Shock Wave Interaction in Hypervelocity Flow,” Ph.D. Thesis, Graduate Aerospace Laboratories of the California Institute of Technology, California Inst. of Technology, Pasadena, CA, 1995.
2. EdneyB. “Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speed in the Presence of Impinging Shocks,” The Aeronautical Research Inst. of Sweden, FFA Rept. 115, Bromma, Sweden, 1968.
3. Type III and type IV shock/shock interferences: theoretical and experimental aspects
4. Numerical study of inviscid shock interactions on double-wedge geometries
5. Numerical Investigation of Shock/Vortex Interaction in Hypersonic Thermochemical Nonequilibrium Flow
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