Experimental investigation of laminar-flow separation on a flat plate induced by deflected trailing-edge flap at Mach 19
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic speed
Harvey, W. D.↗
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Hypersonic aerodynamic characteristics of low-wave-drag elliptical-body-tail combinations as affected by changes in stabilizer configuration
Stabilizer and tail assembly effects on overall aerodynamic characteristics of lifting bodies at hypersonic speeds
Fox, C. H., Jr.↗
Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface at hypersonic speeds
Dearing, J. D.↗
Experimental base pressures on 9 deg spherically blunted cones at Mach numbers from 10.5 to 20
Base pressure measurements at angle of attack for spherically blunted cones at hypersonic speed
Miller, C. G., III↗
Engineering considerations on the transversal contour of a lifting body.
Lift drag ratios attainable by slender bodies at hypersonic speeds assuming modified Newtonian pressure distribution and surface constant friction coefficient
Huang, H.-Y.↗
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.↗
Heat-transfer and pressure distributions inside the hinge-line gap of a wedge-flap combination at Mach number 10.4
Heat transfer and pressure distributions inside hinge line gap of wedge-flap combination at hypersonic speeds
Dearing, J. D.↗
Theoretical considerations of some nonlinear aspects of hypersonic panel flutter Annual report, 1 Sep. 1966 - 31 Aug. 1967
Systematic investigation of effects on panel response and stability of nonlinear aerodynamic loading at hypersonic speeds
Mc Intosh, S. C.↗
Proceedings of the Conference on the Role of Simulation in Space Technology, part B
Simulation studies and facilities for atmospheric reentry at hypersonic speeds
Source record↗
Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10
Laminar heat transfer distributions for blunted- cone, cone frustum reentry configuration at hypersonic speed using Reynolds number
Dearing, J. D.↗
A modified method of integral relations approach to the blunt-body equilibrium air flow field, including comparisons with inverse solutions
Numerical calculation of inviscid adiabatic flow field around blunt bodies at hypersonic speeds
Garrett, L. B.↗
Boundary-layer tripping with emphasis on hypersonic flows.
Boundary layer trip geometry, size and location effects on position of transition at hypersonic speeds
Morrisette, E. L.↗
Some aspects of aerodynamic heating
Aerodynamic heating of blunt body at hypersonic speeds
Truitt, R. W.↗
An experimental investigation of boundary- layer transition on a 10 deg half-angle cone at Mach 6.9
Boundary layer transition on nose cones at hypersonic speeds
Fischer, M. C.↗
Turbulent-boundary-layer heat-transfer and transition measurements with surface cooling at Mach 6
Wall cooling effects on turbulent heat transfer and boundary layer transition for sharp leading edge flat plate at hypersonic speeds
Cary, A. M., Jr.↗
Transitional and turbulent heat transfer correlations for a lifting entry vehicle at Mach 10
Applicability of boundary layer transition and turbulent heat transfer data for lifting reentry vehicle at hypersonic speed to space shuttles
Reda, D. C.↗
The hypersonic viscous shock-layer problem
Laminar flow past axisymmetric blunt bodies moving at hypersonic speed
Davis, R. T.↗
Theoretical considerations of some nonlinear aspects of hypersonic panel flutter Annual report, 1 Sep. 1967 - 31 Aug. 1968
Stability and postcritical response of infinite width panels on hinged supports due to aerodynamic loads at hypersonic speed
Lerner, J. I.↗