Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight

Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight

著者名:

M. Takahashi ( Japan Aerospace Exploration Agency, Kakuda, Miyagi, Japan )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

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

シリーズ巻号:

2008

発行年:

2008

通号:

2008-2549

ペーパー番号:

AIAA Paper 2008-2549

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200804 [CD-ROM 2008 Disc 4]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049522
シリーズID:	PA00000152
会議名:	AIAA International Space Planes and Hypersonic Systems and Technologies Conference
回次:	15th
会議開催地:	Dayton, OH
会議開催年:	2008.04.28-2008.05.01
論文注記:	15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 28 April - 1 May 2008, Dayton, Ohio

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1 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	7 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
2 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	8 テクニカルペーパー Viscous Drag Reduction in a Mach 12 Scramjet Engine Rowan, S., Takahashi, M., Sunami, T., Itoh, K., Komuro, T., Sato, K. American Institute of Aeronautics and Astronautics
3 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	9 テクニカルペーパー Experimental study on flow establishment in a large scale scramjet Tanno,H., Komuro,T., Sato,K., Ueda,S., Itoh,K. American Institute of Aeronautics and Astronautics
4 国際会議録 Scramjet Combustor Characteristics at Hypervelocity Condition over Mach 10 Flight M. Takahashi, T. Komuro, K. Sato ESA Communication Production Office	10 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
5 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	11 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
6 テクニカルペーパー Ignition Transient Phenomena in a Scramjet Engine at Mach 12 Flight Condition M. Kodera, V. Yang, M. Takahashi, K. Itoh American Institute of Aeronautics and Astronautics	12 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

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