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↗
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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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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↗
Numerical computation of flow past a scalariform cone
Numerical computation of uniform flow past scalariform circular cone immersed in supersonic stream of ideal gas
IDEAL GAS↗
Convective heat transfer to a lifting flat-faced-cone entry body
Convective heat transfer and pressure distribution measurements on lifting blunt cone reentry body
LIFTING BODY↗
Study of local flow conditions over a hemispherically blunted 25 deg cone for a shallow re-entry trajectory
Local flow conditions over hemispherically blunted 25 deg cone for shallow reentry trajectory
BLUNT BODY↗
Wedge and cone theory for m infinity equals infinity.
Tabulated values of ratio of cone surface pressure-pressure at shock
CONE↗
Boundary-layer transition on ablating cones at speeds up to 7 km/sec.
Laminar and turbulent boundary layer flow in ablating cones in hypervelocity flight
HIGH SPEED FLYING↗
Comment on the location of the center of pressure of a right circular cone using Newtonian impact theory.
Static pitching moment coefficient determination from location of center of pressure in right circular cone, using Newtonian impact mechanics
IMPACT PRESSURE↗
Boundary-layer transition on ablating cones at speeds up to 7 km/sec.
Laminar and turbulent boundary layer flow in ablating cones in hypervelocity flight
TURBULENT BOUNDARY LAYER↗
High-amplitude dynamic-stability characteristics of blunt 10-degree cones
High amplitude, dynamic stability characteristics of blunt 10-degree cones
CONE↗
Evaluation of the cone radiometer
Cone radiometer evaluation, and its application as measuring apparatus of incidence light flux
RADIOMETER↗
Pressure distribution measurements on cones
Pressure distribution measurements on cones in symmetrical incompressible flow, with and without influence of wake
CONE↗