H. H. Hamilton

Approximate method of predicting heating on the windward side of Space Shuttle Orbiter and comparisons with flight data

H. H. Hamilton, H. Hamilton, 1982 .

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

H. H. Hamilton, J. D. Dearing, 1968 .

Calculation of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data

K. J. Weilmuenster, H. H. Hamilton, K. Weilmuenster, 1983 .

Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue

H. H. Hamilton, 1980 .

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

H. H. Hamilton, J. D. Dearing, 1968 .

A hybridized method for computing high-Reynolds-number hypersonic flow about blunt bodies

K. J. Weilmuenster, H. H. Hamilton, 1979 .

A review of preflight estimates of real-gas effects on space shuttle aerodynamic characteristics

J. P. Arrington, H. H. Hamilton, W. C. Woods, 1983 .