Stall Detection on a Leading-Edge Plasma Actuated Pitching Airfoil Utilizing Onboard Measurement
- Author(s):
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2009
- Pub. Year:
- 2009
- No.:
- 2009-0093
- Paper no.:
- AIAA Paper 2009-0093
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200901
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Separation Control Using Plasma Actuators: Dynamic Stall Control on an Oscillating Airfoil
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap
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 |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |