Flow-field characteristics and normal-force correlations for delta wings from Mach 2.4 to 4.6
27th Aerospace Sciences Meeting ; 1989 ; Reno , NV , U.S.A.
1989-01-01
Conference paper
Electronic Resource
English
Aerodynamics , NASA Langley , Vortices , Sweep Angle , Camber , Swept Wing , Wind Tunnels , Bow Shock