On the Performance of AUSM Based Schemes in Hypersonic Flow with Equilibrium Gas Effects
- 著者名:
- H. Vafadar Moradi ( Iran University of Science and Technology, Tehran, Iran )
- M. Hosseinalipour
- 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:
- 2006-7962
- ペーパー番号:
- AIAA Paper 2006-7962
- 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
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
4
テクニカルペーパー
Numerical analysis of hypersonic viscous flow around a blunt body using Roe's FDS and AUSM+ schemes
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
Modeling of Transition Effects in Hypersonic Intake Flows Using a Correlation-Based Intermittency Model
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
A hot dynamic seal rig for measuring hypersonic engine seal durability and flow performance
National Aeronautics and Space Adminstration |