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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 unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 degree half-angle cone at Mach 8
Experimental surface pressure distributions on spherically blunted cone at Mach numbers from 1.50 to 4.63
Experimental pressure distributions on 120 deg cone at Mach 2.96 to 4.63 and angles of attack from 0 deg to 20 deg
Calorimetric efficiency of cone and column solar energy concentrator
Base pressure distribution on blunted cones during supersonic wind tunnel tests
Newtonian aerodynamics for circular cones modified to produce lift at zero angle of attack
Shock shape and surface pressure measurements on hypersonic pointed cones in helium
Supersonic flow characteristics in wake of blunt cones
Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies
Upwash patterns on ablating and nonablating cones at hypersonic speeds
Aerodynamic characteristics of large-angle cones in supersonic lifting capabilities
Flow model for vortex shedding from slender body in coning motion
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