Laminar Flow Control on a Swept Wing with Distributed Roughness
- Author(s):
- A. Carpenter ( Texas A&M University, College Station, TX )
- W. Saric,
- H. Reed
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- 2008
- Pub. Year:
- 2008
- No.:
- 2008-6901
- Paper no.:
- AIAA 2008-6901
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200810 [CD-ROM 2008 Disc 10]
- Type:
- Technical Paper
Similar Items:
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 |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
In-Flight Receptivity Experiments on a 30-Degree Swept-Wing using Micron-Sized Discrete Roughness Elements
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Application of Variable Leading-Edge Roughness for Transition Control on Swept Wings
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 |