Combined effects of mass addition and nose bluntness on boundary-layer transition.
Cone boundary layer transition location and Reynolds number as function of nose bluntness combined effect with Ar, air and He mass injection
Akin, C. M.↗
Engineering topics
Marvin, J. G.
Publications and source records attributed to Marvin, J. G..
A study of the nonsimilar nature of the laminar boundary layer in a region of adverse pressure gradient.
Nonsimilar laminar boundary layer solutions with negative pressure gradient compared to experimental boundary layer velocity profiles, momentum and displacement thicknesses
Gallo, W. F.↗
Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5
Integer relations method of determining inviscid shock layer flow and pressure distributions over blunt bodies
Inouye, M.↗
Convective heating in regions of large favorable pressure gradient.
Convective heating in shoulder regions of flat- faced cylinder with large favorable pressure gradient
HEAT SHIELD↗
Comparison of convective stagnation heat transfer in air, CO2-N2, and CO2-Ar gas mixtures
Convective stagnation heat transfer of carbon dioxide, nitrogen-argon gas mixtures compared to air in shock tube tests
Akin, C. M.↗
Laminar convective heating and ablation in the Mars atmosphere.
Mars atmospheric composition and laminar convective heating and ablation studied to predict performance of heat protection systems during entry
LAMINAR HEAT TRANSFER↗
Convective heating in regions of large favorable pressure gradient.
Convective heating in shoulder regions of flat- faced cylinder with large favorable pressure gradient
CONVECTIVE HEAT TRANSFER↗
Convective heat transfer in planetary gases.
Heating rates in gas mixtures of planetary atmospheres predicted by equation using transport properties of gases at lower temperatures
STAGNATION TEMPERATURE↗
Laminar convective heating and ablation in the Mars atmosphere.
Mars atmospheric composition and laminar convective heating and ablation studied to predict performance of heat protection systems during entry
MARS ATMOSPHERE↗
Pressure and convective heat-transfer measure- ments in a shock tunnel using several test gases
Pressure and convective heat-transfer measurements on hemisphere-cylinder, blunted 30 degree cone, in shock tunnel using several test gases
BLUNT BODY↗
Convective heat transfer in planetary gases
Equilibrium convective heat transfer in air, nitrogen, hydrogen, carbon dioxide and argon
CONVECTIVE HEAT TRANSFER↗
Pressure and heat-transfer distribution on the afterbody of a lifting Mercury- type capsule at Mach number 15 in helium
Afterbody pressure and heat transfer distribution, shock wave shapes, and photographs of local flow conditions for Mercury type capsule at Mach number 15 in helium
AFTERBODY↗