Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.
Hypersonic flow distribution and separation types over highly swept delta wings with trailing edge flaps at Mach 6
Keyes, J. W.↗
Engineering topics
Keyes, J. W.
Publications and source records attributed to Keyes, J. W..
Turbulent heat transfer associated with control surface at Mach 6.
Turbulent heat transfer associated with controls for attached or separated flow analyzed for design of hypersonic cruise aircraft
Emery, J. C.↗
Flow phenomena and separation over highly swept delta wings with trailing-edge flaps at Mach 6.
Hypersonic flow distribution and separation types over highly swept delta wings with trailing edge flaps at Mach 6
Keyes, J. W.↗
Calculated and experimental hinge moments on a trailing-edge flap of a 75 deg swept delta wing at Mach 6
Calculated and experimental hinge moments on trailing-edge flaps of swept delta wings at hypersonic speeds and positive deflection angles
Ashby, G. C., Jr.↗
Effect of forward-facing jets on aerodynamic characteristics of blunt configurations at Mach 6.
Forward facing jets effect on blunt configurations aerodynamic characteristics from wind tunnel tests at Mach 6, emphasizing drag increase
HYPERSONIC WIND TUNNEL↗