Passive control of flow separation over delta wings at high angle-of-attack
- Author(s):
Van Dyken, R. ( Naval Air Warfare Center Weapons Division ) Yu, K. Gutmark, E. Tuncer, I. Platzer, M. McLachlan, B. Bell, J. - Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-0661
- Paper no.:
- 96-0661
- Page(from):
- 1
- Page(to):
- 8
- 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 |
7
Technical Paper
Simple wings unsteady aerodynamics at high angles of attack: experimental and modeling results
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
A computational study of flow separation characteristics and wake profiles behind a flapping airfoil
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Juncture fillets for vortex flow control on double-delta wings undergoing sideslip
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
A Computational Study of Flow Separation Characteristics and Wake Profiles Behind a Flapping Airfoil
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Computational Investigation of Asymmetric Vortical Flow Characteristics at High Angle of Attack
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
PMARC potential flow solutions with wakes over an ogive cylinder at high incidence
American Institute of Aeronautics and Astronautics |