High-Lift System for a Supercritical Airfoil: Simplified by Active Flow Control
- Author(s):
- L. Pack-Melton ( NASA Langley Research Center, Hampton, VA )
- N. Schaeffler
- J. Lin
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-0707
- Paper no.:
- AIAA Paper 2007-707
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200703 [CD-ROM 2007 Disc 3]
- 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 |
3
Technical Paper
Analogue/Digital Wind Tunnel Testing of Active Low Momentum Flow Control on Single and Multi-Component Airfoil Systems at High Lift.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Application of Excitation from Multiple Locations on a Simplified High-Lift System
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |