Scramjet Engine Tests at Mach 4 and 6-Reference-Cited by-同舟云学术

Scramjet Engine Tests at Mach 4 and 6

Published:1997 Issue: Volume: Page:147-162
ISSN:0926-5112
Container-title:Fluid Mechanics and Its Applications
language:
Short-container-title:

Author:

Masuya Goro,Chinzei Nobuo,Miki Yoichiro

Publisher

Springer Netherlands

Link

http://link.springer.com/content/pdf/10.1007/978-94-011-5432-1_12

Reference17 articles.

1. Miyajima, H. Chinzei, N., Mitani, T. Wakamatsu, Y, and Maita, M.: Development Status of the NAL Ramjet Engine Test Facility and Sub-Scale Scramjet Engine, AIM Paper 92-5094, 1992.

2. Tani, K., Kanda, T., Kudou, K., Murakami, A., Komuro, T., and Itoh, K.: Aerodynamic Performance of Scramjet Inlet Models with a Single Strut, AIAA Paper 93-0741, 1993.

3. Tani, K., Kanda, T. and Tokunaga, T.: Starting Characteristics of Scramjet Inlets, Proc. Eleventh Int. Sympo. Air Breathing Engines, Tokyo, Japan, Sep. 1993, 1071–1080.

4. Masuya, G., et al.: Some Governing Parameters of Plasma Torch Igniter/Flameholder in a Scramjet Combustor, J. Propulsion and Power 9(1993), 176–181.

5. Masuya, G., Komuro, T., Murakami, A., Shinozaki, N., Nakamura, A., Murayama, M., and Ohwaki, K.: Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts, J. Propulsion and Power 11(1995), 301–307.

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