Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint
- 著者名:
- Asai, K. ( National Aerospace Laboratory, Japan )
- Kanda, H.
- Kunimasu, T.
- Liu, T.
- Sullivan, J.P.
- 掲載資料名:
- AIAA paper
- シリーズ名:
- AIAA Paper : AIAA Advanced Measurement and Ground Testing Technology Conference
- シリーズ巻号:
- 1996
- 発行年:
- 1996
- 通号:
- 96-2185
- ペーパー番号:
- 96-2185
- 開始ページ:
- 1
- 終了ページ:
- 11
- 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:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
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 |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
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
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Global Heat Transfer Measurement in a Hypersonic Shock Tunnel using Temperature-Sensitive Paint.
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |