Measurements of radiative heating on sharp cones.
Free flight measurement of radiative heat load on circular cone and comparison with predicted equilibrium and nonequilibrium radiation
CIRCULAR CONE↗
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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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Force-coefficient and moment-coefficient correlations and air-helium simulation for spherically blunted cones
Force coefficient and moment coefficient correlations and air-helium simulation of spherically blunted cones - hypersonic wind tunnel testing
CONE↗
The effects of nose bluntness on the pressure fluctuations measured on 15 deg and 20 deg cone-cylinders at transonic speeds
Effect of nose bluntness on pressure fluctuations measured on 15 deg and 20 deg cone cylinders at transonic speeds
CYLINDER↗
Maximum lift-drag ratios of delta-wing-half- cone combinations at a mach number of 20 in helium
Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift
DELTA WING↗
Aerodynamic force and moment characteristics of spheres and cones at mach 7.0 in methane-air combustion products
Aerodynamic force and moment characteristics of spheres and cones at hypersonic speeds in methane-air combustion products
HYPERSONIC SPEED↗
Free-flight Cone Dynamic Stability Testing at High Amplitudes of Oscillation
Dynamic stability of slender cones subjected to high oscillation amplitude - measurement in wind tunnels by free flight techniques
FREE FLIGHT TEST APPARATUS↗
Favorable interference effects on maximum lift-drag ratios of half-cone delta-wing configurations at mach 6.86
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
DELTA WING↗
Static stability characteristics of several raked-off circular and elliptical cones at mach 6.7
Static stability characteristics of circular and elliptical cones at hypersonic speeds
HYPERSONIC SPEED↗
Effects of buoyancy on the laminar flow from an isothermal cone rotating in a quiet fluid.
Buoyancy effects on heat transfer to laminar boundary layer from isothermal rotating cone
ROTATING CONE↗
Hypersonic viscous effects on free-flight slender cones.
Wind tunnel free flight testing technique to obtain data on hypersonic viscous effects on slender cones
SLENDER CONE↗
Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0
Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0
MACH NUMBER↗
Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air
Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reynolds numbers
MACH NUMBER↗
Aerodynamic characteristics of the sharp right circular cone at Mach 20.3 and angles of attack to 110 deg in helium
Static longitudinal aerodynamic characteristics of sharp right circular cone at Mach 20.3 and angles of attack to 110 deg in helium
HELIUM↗
Radar cross section and optical radiation from the Trailblazer IIa 9 deg half-angle blunt nose cone during hypersonic reentry
Radar cross sections and optical radiation measurement of blunt nose cone during hypersonic reentry
HYPERSONIC REENTRY↗
Linear Aerodynamic Loads on Cone-Cylinders at Mach Numbers from 0.7 to 2.0
Linear aerodynamic loads for cone-cylinder configurations in trisonic range
CYLINDER↗
Laminar boundary layer on a cone with uniform injection
Laminar compressible boundary layer on cone with uniform injection
CONE↗
Laminar boundary layer on a cone in supersonic flow with uniform mass transfer
Laminar boundary layer solution on cone in supersonic flow with uniform mass transfer
MASS TRANSFER↗
Aerodynamic characteristics of raked-off circular and elliptical cones at a Mach number of 20 in helium
Longitudinal and lateral directional aerodynamic characteristics of raked-off circular and elliptical cones at Mach 20 in helium
REENTRY VEHICLE↗