In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack
- 1 September 1989
- proceedings article
- Published by SAE International
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Experimental investigation of the F/A-18 vortex flows at subsonic through transonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Navier-Stokes solutions about the F/A-18 forebody-LEX configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Numerical simulation of high-incidence flow over the F-18 fuselage forebodyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Wind-Tunnel Investigation of the Forebody Aerodynamics of a Vortex-Lift Fighter Configuration at High Angles of AttackSAE International Journal of Advances and Current Practices in Mobility, 1988
- An airborne system for vortex flow visualization on the F-18 high-alpha research vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Flow visualization techniques applied to full-scale vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Flow visualization from the ground upPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Self-induced wing rock of slender delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981