Swept-Wing Laminar Flow Control Studies Using Cessna O-2A Test Aircraft
- Author(s):
- M. Martin ( Northrop Grumman Corporation, Palmdale, CA )
- A. Carpenter ( Texas A&M University, College Station, TX )
- W. Saric
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : U.S. Air Force T&E Days
- Ser. no.:
- 2008
- Pub. Year:
- 2008
- No.:
- 2008-1636
- Paper no.:
- AIAA Paper 2008-1636
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200802 [CD-ROM 2008 Disc 2]
- Type:
- Technical Paper
Similar Items:
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 |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Development and Testing of a Wing Morphing Mechanism for the Control of a Swept Wing Tailless Aircraft.
Society of Automotive Engineers |
5
Technical Paper
In-Flight Receptivity Experiments on a 30-Degree Swept-Wing using Micron-Sized Discrete Roughness Elements
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
12
Technical Paper
Advanced Laminar Flow Control on a Swept Wing: Useful Crossflow Vortices and Suction (Invited)
American Institute of Aeronautics and Astronautics |