Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flow

Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data

J. L. Hunt, Richard A. Jones · NASA Technical Reports Server (NASA) · 1966 · 47 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +16

Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.

Allen H. Whitehead, J. W. Keyes · AIAA Journal · 1968 · 35 citations

Engineering, Aerospace Engineering, Mechanical Engineering +6

A Simple Method for Determining Heat Transfer, Skin Friction, and Boundary-Layer Thickness for Hypersonic Laminar Boundary-Layer Flows in a Pressure Gradient

M. H. Bertram, W. V. Feller · NASA Technical Reports Server (NASA) · 1959 · 23 citations · Full text

Engineering, Aerospace Engineering, Physics +17

Investigation of the leeward side of a delta wing at hypersonic speeds.

E. J. Cross, W. L. Hankey · Journal of Spacecraft and Rockets · 1969 · 21 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Effect of vortices on delta wing lee-side heating at Mach 6

Allen H. Whitehead · AIAA Journal · 1970 · 15 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14