Full-scale high angle-of-attack tests of an F/A-18
- 22 June 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Analysis of a pneumatic forebody flow control concept about a full aircraft geometryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Forebody vortex flow control on the F-16C using tangential slot and jet nozzle blowingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- X-29 forebody jet blowingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Forebody vortex control using slot blowingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Wind tunnel investigation of aerodynamic and tail buffet characteristics of leading-edge extension modifications to the F/A-18Published by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Numerical prediction of the unsteady flowfield around the F-18 aircraft at large incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- A two camera video imaging system with application to parafoil angleof attack measurementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Numerical simulation of high-incidence flow over the F-18 fuselage forebodyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989