Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition

Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition

著者名:

Takahashi, M. ( Japan Aerospace Exploration Agency, Kakuda, 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:

13th

発行年:

2005

通号:

2005-3350

ペーパー番号:

AIAA Paper 2005-3350

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200508 [CD-ROM 2005 Disc 8]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001623
シリーズID:	PA00000152
会議名:	AIAA/CIRA International Space Planes and Hypersonics Systems and Technologies Conference
回次:	13th
会議開催地:	Capua, Italy
会議開催年:	2005.05.16-2005.05.20

類似資料:

1 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	7 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
2 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	8 テクニカルペーパー Mach 8 Ground Tests of the Hypermixer Scramjet for HyShot-IV Flight Experiment T. Sunami, K. Itoh, K. Satoh, T. Komuro American Institute of Aeronautics and Astronautics
3 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	9 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
4 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	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 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	11 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
6 テクニカルペーパー Numerical Simulation of a Scramjet Engine for JAXA痴 Flight Experiment Using Hyshot Kodera, M., Sunami, T., Itoh, K. 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

1

2

3

4

5

6

7

8

9

10

11

12