Comparison of Stability of Hypersonic Rectangular and Three-Dimensional Inlets to Unsteady Perturbations Using Entropy Considerations
Author:
Affiliation:
1. University of Maryland, College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3363
Reference19 articles.
1. Designing hypersonic inlets for bow shock location control
2. Unsteady characteristics of a hypersonic type IV shock interaction
3. Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow
4. Weiting, A.R. "Experimental Study of Shock Waves Interference Heating on a Cylindrical Leading Edge." PhD Dissertation,Old Dominion University, 1987; alsoNASA TM-100484, May 1987.
5. Edney, B. "Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock, " FFA Report 115, Aeronautical Research Institute of Sweden, 1968.
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