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Modified water-cooled scramjet engine tested under M8 Condition

  • Published:2001-07-08 Issue: Volume: Page:
  • ISSN:
  • Container-title:37th Joint Propulsion Conference and Exhibit
  • language:
  • Short-container-title:

Author:

Kobayashi Kan1,Tomioka Sadatake1,Kanda Takeshi1,Tani Kouichiro1,Hiraiwa Tetsuo1,Saito Toshihito1

Affiliation:

1. National Aerospace Lab., Kakuda, Japan

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Sunami, T., Sakuranaka, N., Tani, K., Hiraiwa, T, and Shimura,T. "Mach 4 Tests of aScramjet Engine - Effects ofIsolator,"ISABEpaper 97-7088,1997.

2. Mach 6 Testing of a Scramjet Engine Model

3. Saito, T., Wakamatsu, Y, Mitani, T., Chinzei, N., and Shimura, T. "Mach 8 Testing of a Scramjet EngineModel,"ISTSpaper 96-a-2-ll, 1996.

4. Testing of a scramjet engine with a strut in M8 flight conditions

5. Mach 8 Testing of a Scramjet Engine Model

Cited by 4 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. 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

2. Evaluation of Thrust Performance in Scramjet Engines with Measured Internal Drag;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

3. Three-Component Force Measurements for Scramjet Engines 1) Engine Drag from Mach 4 to Mach 8 Flight Conditions;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

4. Force Measurements of Fixed-Geometry Scramjet Engines from Mach 4 to 8 Flight Conditions;AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference;2002-06-26
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