Testing of a scramjet engine model in Mach 6 vitiated air flow

Testing of a scramjet engine model in Mach 6 vitiated air flow

著者名:

Hiraiwa, Tetsuo ( National Aerospace Laboratory, Kakuda Research Center, Japan )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

1997

発行年:

1997

通号:

97-0292

ペーパー番号:

97-0292

開始ページ:

1

終了ページ:

11

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050850
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	35th
会議開催地:	Reno, NV
会議開催年:	1997.01.06-1997.01.10
論文注記:	35th Aerospace Sciences Meeting & Exhibit, January 6-10, 1997/Reno, NV

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1 テクニカルペーパー Scramjet engine testing in Mach 6 vitiated air Mitani, T., Hiraiwa, T., Sato, S., Tomioka, S., Kanda, T., Saito, T., Sunami, T., Tani, K. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Mach 6 testing of a scramjet engine model Kanda, Takeshi, Saito, Toshihito, Kudo, Kenji, Komuro, Tomoyuki, Ono, Fumiei, Matsui, Atsushi American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Testing of a scramjet engine with a strut in M8 flight conditions Tomioka, Sadatake, Kanda, Takeshi, Tani, Kouichiro, Mitani, Tohru, Shimura, Takashi, Chinzei, Nobuo American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Experiments on a Scramjet Engine with Ramp-Compression Inlet at Mach 8 Condition. Hiraiwa, T., Kanda, T., Mitani, T., Enomoto, Y. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Scramjet inlet flow computations by hybrid grid method Hiraiwa, Tetsuo, Kanda, Takeshi, Mitani, Tohru American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Similarity parameters of pre-ignition flowfields in a supersonic combustor Zamma, Yoshihiko, Shiba, Hiroyuki, Masuya, Goro, Tomioka, Sadatake, Hiraiwa, Tetsuo, Mitani, Tohru American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Measurements of scramjet engine performance by gas sampling Mitani, Tohru, Takahashi, Masahiro, Tomioka, Sadatake, Hiraiwa, Tetsuo, Tani, Kouichiro American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Auto ignition in a supersonic combustor with perpendicular injection behind backward-facing step Tomioka, Sadatake, Hiraiwa, Tetsuo, Mitani, Tohru, Zamma, Yoshihiko, Shiba, Hiroyuki, Masuya, Goro American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Geometrical effects to aerodynamic performance of scramjet engine Tani, Kouichiro, Kanda, Takeshi, Sunami, Tetsuji, Hiraiwa, Tetsuo, Tomioka, Sadatake American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Gas-sampling Survey from Exhaust Flows in Scramjet Engines at Mach-6 Flight Condition Hiraiwa, T., Kobayashi, K., Tomioka, S., Izumikawa, M., Watanabe, S. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Scramjet engine test at Mach 6 flight condition Sato, S., Izumikawa, M., Tomioka, S., Mitani, T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Modified Water-cooled Scramjet Engine Tested under M8 Condition Kobayashi,K., Tomioka,S., Kanda,T., Tani,K., Hiraiwa,T., Saito,T. American Institute of Aeronautics and Astronautics

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