Supersonic Flow Choking in Engine Wind Tunnels
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/55/636/55_636_43/_pdf
Reference12 articles.
1. 1) Chinzei, N., Mitani, T. and Yatsuyanagi, N.: Scramjet Engine Research in the National Aerospace Laboratory in Japan, Scramjet Propulsion, Curran, E. T. and Murthy, S. N. B., eds., AIAA, Reston, VA, 2000, pp. 159–222.
2. Boundary-Layer Control in Mach 4 and Mach 6 Scramjet Engines
3. 3) Mitani, T., Tomioka, S., Kanda, T., Chinzei, N. and Kouchi, T.: Scramjet Performance Achieved in Engine Tests from M6 to M8 Flight Condition, AIAA Paper 2003-7009, 12th AIAA Spaceplane and Hypersonic Systems and Technologies, Norfolk, VA, 2003.
4. 4) Ueda, S., Tomioka, S., Ono, F., Sakuranaka, N., Tani, K. and Murakami, A.: Mach 6 Test of a Scramjet Engine with Multi-Staged Fuel Injection, AIAA Paper 2006-1027, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 2006.
5. 5) 三谷徹,他:小型風洞とエンジン補完実験,航技研報告TR-1458,2003, p. 227.
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