Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges, part II: receptivity to sound
- 著者名:
- Zhong, Xiaolin ( University of California, Los Angeles )
- 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:
- 97-0756
- ペーパー番号:
- 97-0756
- 開始ページ:
- 1
- 終了ページ:
- 19
- 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 |
7
テクニカルペーパー
Numerical Simulation of Hypersonic Boundary Layer Receptivity and Stability on Blunt Circular Cones
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
Direct numerical simulation of 3-D hypersonic boundary layer receptivity to freestream disturbances
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
テクニカルペーパー
Numerical Simulation of Receptivity and Stability of Nonequilibrium Reacting Hypersonic Boundary Layers
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
Direct Numerical Simulation and the Theory of Receptivity in a Hypersonic Boundary Layer
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Direct Numerical Simulation of Instability of Nonequilibrium Reacting Hypersonic Boundary Layers
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
High-order semi-implicit simulation of hypersonic boundary layer stability and transition
American Institute of Aeronautics and Astronautics |