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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Wind tunnel calibration of 30 deg included angle cone for determination of local values of Mach number, total pressure, and flow distribution
Supersonic aerodynamics of large angle cones
Hypersonic heat transfer and pressure distribution on spherically blunted cone
Base pressure measurements at angle of attack for spherically blunted cones at hypersonic speed
Cone-cylinder models tested in supersonic wind tunnel to evaluate effect of wall reflected disturbances on model pressure distributions
Cup and cone tensile fractures in quenched and tempered plate steel
Weak locally homogeneous turbulence in idealized distorting mean flow in cone, obtaining two point correlation equations
Ablation patterns on cones having laminar and turbulent flows from ballistic range boundary layer transition studies using ablative models
Angle of attack effect on laminar boundary layer transition on slender cone in contoured nozzle of helium tunnel, discussing Reynolds and Mach numbers effect
Hypersonic surface measurements and flowfield properties about slender cones in hypersonic viscous interaction regime
Subliming ablation effects on boundary layer transition for cones in hypersonic flow, discussing Reynolds numbers measured in wind tunnel tests
Transition from laminar to turbulent boundary layer flow on sharp cones hypersonic Mach numbers, noting measurement techniques
Cup and cone tensile fractures in quenched and tempered plate steel
Approximate method to predict ablative recession rate and mass loss on sphere cones in Martian atmosphere entry
Sandwich cylinders and cones axial compression general instability buckling loads
Explicit construction of Poincare group generators of proper inhomogeneous Lorentz group for spin-zero and spin-1/2 particles on light cone
Effects of angle of attack and bluntness on shock layer properties of cones at supersonic speeds
Pressure, force, and dynamic stability tests on spherically blunted cones, and comparison with calculated aerodynamic coefficients