Solution of axisymmetric and two-dimensional inviscid flow over blunt bodies by the method of lines

von Hamilton, H. Harris
Veröffentlicht 1978

Heat-transfer and pressure distributions inside the hinge-line gap of a wedge-flap combination at Mach number 10.4

von Dearing, J. David
Veröffentlicht 1968

Experimental investigation of boundary-layer transition on a cooled 7.5° total-angle cone at Mach 10

von Everhart, Philip E.
Veröffentlicht 1967

Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies

von Hamilton, H. Harris
Veröffentlicht 1980

Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4

von Hamilton, H. Harris
Veröffentlicht 1968

A hybridized method for computing High-Reynolds-Number hypersonic flow about blunt bodies

von Weilmuenster, K. James
Veröffentlicht 1979