Film Cooling Effectiveness in High Enthalpy Flows

Author:

Mizoguchi Makoto,Iwata Naoko,Hayashi Kentaro,Aso Shigeru,Tani Yasuhiro

Publisher

Japan Society for Aeronautical and Space Sciences

Reference20 articles.

1. 1) 久保田弘敏,鈴木宏二郎,綿貫忠晴:宇宙飛行体の熱気体力学,東京大学出版会,東京,2002, pp. 97–166.

2. A Study on Reduction of Aerodynamic Heating by Opposing Jet in Supersonic Flow

3. 3) Dannenberg, R. E.: Helium Film Cooling on a Hemisphere at a Mach Number of 10, NASA TN D-1550, 1962.

4. An experimental investigation of turbulent slot injection at Mach 6

5. 5) Aso, S., Kurotaki, T., Miyamoto, Y., Isomura, Y., Kurosaki, R. and Katayama, M.: Experimental and Computational Study on Reduction of Aerodynamic Heating Load by Film Cooling in Hypersonic Flows, AIAA Paper 97-0770, 1997.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Influence of Coolant Gas Properties on Film Cooling Effectiveness in High Enthalpy Flows;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

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