Measurement of Mass Capture Ratio of Scramjet Inlet Models
Author:
Affiliation:
1. National Aerospace Laboratory of Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-11
Reference24 articles.
1. Mach 6 Testing of a Scramjet Engine Model
2. Scramjet engine test at the Mach 6 flight condition
3. Tani, K., Kanda, T., Sunami, T., Hiraiwa, T., and Tomioka, S. "Geometrical Effects to Aerodynamic Performance of Scramjet Engine,"AIAAPaper97-3018,Jul.1997.
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