Steady and unsteady terminal shock aerodynamics on cone cylinder bodies
Effects of shock induced boundary layer separation on cone cylinder body aerodynamics
Ericsson, L. E.↗
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Static aerodynamic characteristics of blunted cones in the Mach-number range from 2.2 to 9.5
Static aerodynamic characteristics of blunted cones in Mach number range 2.2 to 9.5
Walker, B. J.↗
Static aerodynamic characteristics of three blunted sixty-degree half-angle cones at Mach numbers from 0.60 to 1.30
Subsonic and transonic static aerodynamic characteristics data on 60 deg half-angle cones
Marko, W. J.↗
Aerodynamic characteristics of two blunt, half-cone wedge entry configurations at Mach numbers from 2.30 to 4.63
Aerodynamic characteristics of two blunt half cone wedge entry configurations at supersonic speeds
Foster, G. V.↗
Calibration of 30 deg included-angle cone for determining local flow conditions in Mach number range of 1.51 to 3.51
Wind tunnel calibration of 30 deg included angle cone for determination of local values of Mach number, total pressure, and flow distribution
Vahl, W. A.↗
Supersonic aerodynamics of large-angle cones
Supersonic aerodynamics of large angle cones
Campbell, J. F.↗
Heat transfer and pressure distributions on spherically blunted 25 deg half-angle cone at Mach 8 and angles of attack up to 90 deg
Hypersonic heat transfer and pressure distribution on spherically blunted cone
Bushnell, D. M.↗
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↗
Blockage effects of cone-cylinder bodies on perforated wind tunnel wall interference
Cone-cylinder models tested in supersonic wind tunnel to evaluate effect of wall reflected disturbances on model pressure distributions
Mitchell, G. A.↗
The split, layered, cup-and-cone tensile fracture.
Cup and cone tensile fractures in quenched and tempered plate steel
Clough, W. R.↗
Weak locally homogeneous turbulence in idealized flow through a cone.
Weak locally homogeneous turbulence in idealized distorting mean flow in cone, obtaining two point correlation equations
Deissler, R. G.↗
Ablation patterns on cones having laminar and turbulent flows.
Ablation patterns on cones having laminar and turbulent flows from ballistic range boundary layer transition studies using ablative models
Canning, T. N.↗
Hypersonic transition studies on a slender cone at small angles of attack.
Angle of attack effect on laminar boundary layer transition on slender cone in contoured nozzle of helium tunnel, discussing Reynolds and Mach numbers effect
Henderson, A., Jr.↗
Hypersonic viscous interaction on slender cones.
Hypersonic surface measurements and flowfield properties about slender cones in hypersonic viscous interaction regime
Horstman, C. C.↗
Unusual boundary-layer transition results on cones in hypersonic flow.
Subliming ablation effects on boundary layer transition for cones in hypersonic flow, discussing Reynolds numbers measured in wind tunnel tests
Larson, H. K.↗
Boundary-layer transition on sharp cones at hypersonic Mach numbers.
Transition from laminar to turbulent boundary layer flow on sharp cones hypersonic Mach numbers, noting measurement techniques
Henderson, A., Jr.↗
The split, layered, cup-and-cone tensile fracture.
Cup and cone tensile fractures in quenched and tempered plate steel
Clough, W. R.↗
Ablative surface recession and mass loss on large-angle sphere-cones.
Approximate method to predict ablative recession rate and mass loss on sphere cones in Martian atmosphere entry
Orlik-Rueckemann, K. J.↗