Flight Testing of Pneumatic Forebody Vortex Control on the X-29 Technology Demonstrator
- 1 October 1992
- proceedings article
- Published by SAE International
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Flight simulation and data analysis during a high angle of attack vortex flow control flight test programPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- High angle-of-attack control enhancement on a forward swept wing aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- An experimental study of pneumatic vortex flow control on high angleof attack forebody modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- X-29 forebody jet blowingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Control of Forebody Vortex Orientation to Enhance Departure Recovery of Fighter AircraftJournal of Aircraft, 1982