Effects of Active Control on the Structure of Flow in a Supersonic Jet
- Author(s):
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Flow Control Conference
- Ser. no.:
- 2008
- Pub. Year:
- 2008
- No.:
- 2008-3876
- Paper no.:
- AIAA Paper 2008-3876
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200807 [CD-ROM 2008 Disc 7]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Active noise control in jets from conical and contoured supersonic nozzles with plasma actuators
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Active Control of High Speed and High Reynolds Number Free Jets Using Plasma Actuators
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Effects of Nozzle Trailing Edge Modifications on Noise Radiation in a Supersonic Rectangular Jet
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Flow and Noise Control in High Speed and High Reynolds Number Jets Using Plasma Actuators
American Institute of Aeronautics and Astronautics |