Numerical and experimental analysis of a hypersonic variable geometry inlet
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-899
Reference11 articles.
1. Scuderi, L.F., Orton, G. F., Hunt, J.L. "Mach 10 Cruise/Space Access Vehicle Definition," AIAA Paper 98-1584, 8& International Space Planes Conference, April, 98.
2. High-Speed Viscous Corner Flow
3. Supersonic interference flow along the corner of intersecting wedges.
4. Supersonic Interaction in the Corner of Intersecting Wedges at High Reynolds Numbers
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2. Shock Control Method for Hypersonic Inlets Based on Forebody Secondary Flow Recirculation;AIAA Journal;2018-06
3. Ramp Shock Regulation of Supersonic Inlet with Shape Memory Alloy Plate;AIAA Journal;2018-04
4. Experimental and Numerical Investigation of a Fluidically Variable Hypersonic Inlet;AIAA Journal;2017-08
5. Numerical investigation of two-dimensional supersonic variable-geometry inlet for ramjet;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02
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