Experimental study on flow establishment in a large scale scramjet

Experimental study on flow establishment in a large scale scramjet

著者名:

Tanno,H. ( NAL Kakuda Space Propulsion Laboratory )
Komuro,T.
Sato,K.
Ueda,S.
Itoh,K.

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference

シリーズ巻号:

2001

発行年:

2001

通号:

2001-1889

ペーパー番号:

AIAA-2001-1889

開始ページ:

1

終了ページ:

6

総ページ数:

6

出版情報:

Reston, VA: 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:	ZA00050819
シリーズID:	PA00000152
会議名:	AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference
回次:	10th
会議開催地:	Kyoto, Japan
会議開催年:	2001.04.24-2001.04.27
論文注記:	AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference 24-27 April 2001 Kyoto, Japan

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1 テクニカルペーパー Numerical Analysis of Experimental Results on the Surface Catalycity in HIEST Ueda, S., Sato, K., Komuro, T., Tanno, H., Itoh, K., Kurotaki, T., Ito, T. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Performance Characteristics of Scramjet Engine with Different Combustor Shapes at Hypervelocity Condition over Mach 10 Flight M. Takahashi, T. Komuro, K. Sato, M. Kodera, H. Tanno, K. Itoh American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Hypersonic Aerodynamic Research of HOPE using High Enthalpy Shock Tunnel Itoh,K., Komuro,T., Sato,K., Tanno,H., Ueda,S. American Institute of Aeronautics and Astronautics	8 国際会議録 Experiment on fuel injection in high-enthalpy flow Tanno,H., Komuro,T., Sato,K., Itoh,K., Ueda,S. SPIE-The International Society for Optical Engineering
3 テクニカルペーパー Study on Surface Catalytic Effect using High Enthalpy Shock Tunnel Ueda,S., Sato,K., Komuro,T., Tanno,H., Itoh,K., Shirouzu,M. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Aerodynamic Characteristics of Generic Models Under Real-Gas Condition in the Free-Piston Shock Tunnel HIEST H. Tanno, T. Komuro, K. Sato, K. Itoh,, M. Takahashi American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Laser Absorption Spectroscopy for Determination of Flow Characteristics in High Enthalpy Shock Tunnel H. Tanno, T. Komuro, K. Sato, K. Itoh American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST H. Tanno, K. Sato, T. Komuro, K. Itoh, M. Takahashi American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight M. Takahashi, T. Komuro, K. Sato, M. Kodera, H. Tanno,, K. Itoh American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition Takahashi, M., Sunami, T., Tanno, H., Komuro, T., Kodera, M., Itoh, K. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Effect of Combustor Shape on Scramjet Characteristics at Hypervelocity Condition over Mach 10 Flight M. Takahashi, T. Komuro, K. Sato, M. Kodera, H. Tanno, K. Itoh American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST H. Tanno., T. Komuro, K. Sato, K. Itoh,, M. Takahashi, K. Fujii. American Institute of Aeronautics and Astronautics

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