Oblique modes in attachment-line boundary layer
- Author(s):
- Lin, R.-S. ( High Technology Corporation )
- Malik, M.R.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1999
- Pub. Year:
- 1999
- No.:
- 99-0812
- Paper no.:
- 99-0812
- Page(from):
- 1
- Page(to):
- 10
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Effect of throat heating on critical roughness and the stability of nozzle wall boundary layer
American Institute of Aeronautics and Astronautics |
8
Technical Paper
DNS of Attachment-line/Crossflow Boundary Layer Instability in Supersonic Swept Wing Flows
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Control of corner flow vortices by geometry shaping in mach 2.4 rectangular nozzles
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
Technical Paper
Spatially Developing Secondary Instabilities and Attachment Line Instability in Supersonic Boundary Layers
American Institute of Aeronautics and Astronautics |