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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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Reynolds number and nose bluntness effects on boundary layer transition for hypersonic half angle cone
Beam stiffness determined for thin walled truncated cones under bending loads
Seismic refraction study of internal structure of volcanic cinder cone
Ultra cone system for ultralow noise reception of RF space communication from Mariner 5 during occultation by Venus
Hypersonic surface measurements and flowfield properties about slender cones in hypersonic viscous interaction regime
Matrix theorem giving necessary and sufficient conditions for leaving cone invariant, considering finite dimensional spaces
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Drag coefficients for spheres and sharp cones in rarefied hypersonic air flow obtained in shock tunnel using free flight technique
Subliming ablation effects on boundary layer transition for cones in hypersonic flow, discussing Reynolds numbers measured in wind tunnel tests
Radiation equilibrium temperature measured downstream of transpiration cooled gas flow near slender cone vertex in continuous flow hypersonic tunnel
Incompressible approximation solution of additive drag coefficient and mass flow ratio for inlets with right circular cones
Heat transfer measurements at Mach 10 on total angle cone downstream of air and helium transpiration cooling region
Mach number and oscillation amplitude effects on transonic dynamic stability of half-angle cone planetary entry shapes
Nose cone separation and door ejection systems for Nike-Apache payload housing
Correlation method for estimating pressure distribution over elliptic supersonic cones
Confirming existance of lunar Mach cones by magnetometer data from Explorer 35
Shock-wave shapes and surface pressures on hemisphere and cone cylinders in low density hypersonic flow including ablation
Flow distribution for large angle cones with short spikes in hypersonic laminar flow