Boundary layer transition due to isolated roughness : Shuttle results from the LaRC 20-inch Mach 6 tunnel
- 著者名:
- Berry, Scott A. ( NASA Langley Research Center )
- Bouslog, Stanley A.
- Brauckmann, Gregory J.
- Caram, Jose M.
- 掲載資料名:
- AIAA paper
- シリーズ名:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- シリーズ巻号:
- 1997
- 発行年:
- 1997
- 通号:
- 97-0273
- ペーパー番号:
- 97-0273
- 開始ページ:
- 1
- 終了ページ:
- 14
- 出版情報:
- 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
類似資料:
1
テクニカルペーパー
Isolated roughness induced boundary-layer transition: Shuttle orbit ground tests and flight experience
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
Shuttle Damage/Repair from the Perspective of Hypersonic Boundary Layer Transition - Experimental Results
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
4
テクニカルペーパー
Boundary Layer Stability Calculations of the HIFiRE Flight 1 Vehicle in the LaRC 20-Inch Mach 6 Air Tunnel
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6wind Tunnels.
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |