Considerations on Mixing and Combustion of a Scramjet Engine. Transition Processes from Weak to Intensive Combustion Mode.-Reference-Cited by-同舟云学术

Considerations on Mixing and Combustion of a Scramjet Engine. Transition Processes from Weak to Intensive Combustion Mode.

Published:2002 Issue:576 Volume:50 Page:22-29
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Sunami Tetsuji,Kodera Masatoshi,Nakahashi Kazuhiro

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/50/576/50_576_22/_pdf

Reference14 articles.

1. 1) Yatsuyanagi, N.: Status of Scramjet Engine Research at NAL, 22nd ISTS 2000-a-09v, 2000.

2. 3) Sunami, T., Sakuranaka, N., Tani, K., Hiraiwa, T. and Shimura, T.: Mach 4 Tests of a Scramjet Engine — Effects of Isolator, 13th ISABE 97-7088, 1997.

3. 4) Sato, S., Izumikawa, M., Tomioka, S. and Mitani, T.: Scramjet Engine Test at Mach 6 Flight Condition, AIAA Paper 97-3021, 1997.

4. 5) Kanda, T., Wakamatsu, Y., Ono, F., Kudo, K., Murakami, A. and Izumikawa, M.: Mach 8 Testing of a Scramjet Engine Model, AIAA Paper 99-0617, 1999.

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