Experimental and numerical investigation of two concepts of hypersonic inlet
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1995-2721
Reference9 articles.
1. K. Richey "The U.S. Air Force Hypersonic Technology Program". AIAA-95-6161, 1995.
2. W. Escher "Motive Power for Next Generation Space Transports: Combined Air breathing Plus Rocket Propulsion". AIAA-95-6076, 1995.
3. Meeting the Challenge
4. D.J. Singh, C.A. Trexler, J.A. Hudgens. ''Three-Dimensional Simulation of a Translating Strut Inlet". AIAA-92-0270, 1992.
5. J.A. Hudgens, C.A. Trexler. "Operating Characteristics at Mach 4 of an Inlet Having Forward-Swept, Sidewall-Compression Surfaces".AIAA-92-3101, 1992.
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