Laser Absorption Spectroscopy for Determination of Flow Characteristics in High Enthalpy Shock Tunnel

Laser Absorption Spectroscopy for Determination of Flow Characteristics in High Enthalpy Shock Tunnel

著者名:

H. Tanno ( Japan Aerospace Exploration Agency, Kakuda, Miyagi, Japan )
T. Komuro
K. Sato
K. Itoh

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:

2006

発行年:

2006

通号:

2006-8002

ペーパー番号:

AIAA Paper 2006-8002

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200624 [CD-ROM 2006 Disc 24]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047253
シリーズID:	PA00000152
会議名:	AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
回次:	14th
会議開催地:	Canberra, Australia
会議開催年:	2006.11.06-2006.11.09

類似資料:

1 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	7 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
2 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	8 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
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 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
4 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	10 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
5 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	11 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
6 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	12 テクニカルペーパー Aerothermodynamic and Scramjet Tests in High Enthalpy Shock Tunnel K. Itoh American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12