Buffet and Buffeting Control in Transonic Flow
- Topics:
- Aerospace and Defense
- Tags:
- Aerospace & Defense,
- Manufacturing,
- ONERA
- Source:
- ONERA
FREE Registration is required
Overview: In transonic flow, the shock wave / turbulent boundary layer interaction and flow separations on wing upper surface of a civil aircraft, which induce "buffet", and then structure vibrations, "buffeting", can greatly influence the aerodynamic behavior. The objectives of this study are to decrease the aerodynamic instabilities by control systems, "Vortex Generators" actuators and a new moving part designed by ONERA, "Trailing Edge Deflector".
(Is this item miscategorized? Does it need more tags? Let us know.)
Format: PDF | Size: 2,724KB | Date: Aug 2003 | Pages: 12
People who downloaded this item also downloaded
![]() |
Experimental Investigations of Rotor-Fuselage Aerodynamic Interactions Using a Helicopter Powered Model |



