Author:
Hiraiwa Tetsuo,Mitani Tohru,Kanda Takeshi
Publisher
American Institute of Aeronautics and Astronautics
Cited by
6 articles.
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1. Influence of Gas Injection and Combustion on Start and Characteristics of Inlet;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28
2. Application of Optimization Algorithms to Scramjet Inlet Design;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16
3. Numerical Analysis and Optimization of Two-Dimensional Hypersonic Inlets;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05
4. Scramjet Performance Achieved in Engine Tests from M4 to M8 Flight Conditions;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15
5. Effect of Ingested Boundary Layer on Scramjet Engines' Thrust and Combustion Characteristics;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26