Experimental investigation of sandwich cylinders and cones subjected to axial compression.
Sandwich cylinders and cones axial compression general instability buckling loads
Baker, E. H.↗
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Realization of Poincare-group generators on a light cone.
Explicit construction of Poincare group generators of proper inhomogeneous Lorentz group for spin-zero and spin-1/2 particles on light cone
Peres, A.↗
Effects of angle of attack and bluntness on the shock-layer properties of a 15 deg cone at a Mach number of 10.6
Effects of angle of attack and bluntness on shock layer properties of cones at supersonic speeds
Cleary, J. W.↗
Aerodynamic characteristics of spherically blunted 45-deg half-angle cones
Pressure, force, and dynamic stability tests on spherically blunted cones, and comparison with calculated aerodynamic coefficients
Passamaneck, R.↗
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5 deg half-angle cone at Mach 8
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 degree half-angle cone at Mach 8
Stainback, P. C.↗
Experimental surface-pressure distributions on a 9 deg spherically blunted cone at Mach numbers from 1.50 to 4.63
Experimental surface pressure distributions on spherically blunted cone at Mach numbers from 1.50 to 4.63
Sawyer, W. C.↗
Experimental pressure distributions on a 120 deg cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0 deg to 20 deg
Experimental pressure distributions on 120 deg cone at Mach 2.96 to 4.63 and angles of attack from 0 deg to 20 deg
Stallings, R. L., Jr.↗
Calorimetric evaluation of two cone-column solar-energy concentrations
Calorimetric efficiency of cone and column solar energy concentrator
Rhodes, M. D.↗
Base pressure distribution of two blunted cones at Mach numbers from 0.3 to 0.8 and 1.81 to 3.51
Base pressure distribution on blunted cones during supersonic wind tunnel tests
Kerr, W. R.↗
Newtonian aerodynamics for circular cones modified to produce lift at zero angle of attack
Newtonian aerodynamics for circular cones modified to produce lift at zero angle of attack
Short, B. J.↗
Shock shapes and pressure distributions for large angle pointed cones in helium at Mach numbers of 8 and 20
Shock shape and surface pressure measurements on hypersonic pointed cones in helium
Inouye, M.↗
Experimental flow properties in the wake of a 120 deg cone at Mach number 2.20
Supersonic flow characteristics in wake of blunt cones
Campbell, J. F.↗
Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-Angle Cones with and Without Cylindrical Afterbodies
Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies
Campbell, James F.↗
Upwash patterns on ablating and nonablating cones at hypersonic speeds
Upwash patterns on ablating and nonablating cones at hypersonic speeds
Mc Devitt, J. B.↗
Supersonic lifting capabilities of large-angle cones
Aerodynamic characteristics of large-angle cones in supersonic lifting capabilities
Campbell, J. F.↗
Theoretical study of vortex shedding from bodies of revolution undergoing coning motion
Flow model for vortex shedding from slender body in coning motion
Kuhn, G. D.↗
An experimental investigation on unit Reynolds number and bluntness effects on boundary-layer transition for a 10 deg half- angle cone at M infinity equals 7
Reynolds number and nose bluntness effects on boundary layer transition for hypersonic half angle cone
Fischer, M. C.↗
Analytical and experimental investigation of end-plane rotations of truncated cones under bending loads
Beam stiffness determined for thin walled truncated cones under bending loads
Faison, R. W.↗