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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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Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics of blunt bodies
Skin temperature and surface pressure of blunted cone-cylinder-flare configuration free flight test vehicle to hypersonic speeds
Effects of gas injection on the heat transfer and pressure distributions on slender cones at hypersonic speeds
Effect of changes in base contour on damping in pitch of blunted cone in wind tunnel
Tables for supersonic flow around right circular cones at zero angle of attack
Cooling of nose cone by ejection of hydrogen and helium from its apex at mach 7
Free flight measurement of radiative heat load on circular cone and comparison with predicted equilibrium and nonequilibrium radiation
Force coefficient and moment coefficient correlations and air-helium simulation of spherically blunted cones - hypersonic wind tunnel testing
Effect of nose bluntness on pressure fluctuations measured on 15 deg and 20 deg cone cylinders at transonic speeds
Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift
Aerodynamic force and moment characteristics of spheres and cones at hypersonic speeds in methane-air combustion products
Dynamic stability of slender cones subjected to high oscillation amplitude - measurement in wind tunnels by free flight techniques
Investigation of half-cone delta wing configurations under laminar boundary layer conditions at Mach 6.86 to determine favorable interference effects on maximum lift-drag ratio
Static stability characteristics of circular and elliptical cones at hypersonic speeds
Buoyancy effects on heat transfer to laminar boundary layer from isothermal rotating cone
Wind tunnel free flight testing technique to obtain data on hypersonic viscous effects on slender cones
Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0
Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reynolds numbers