Add to ORKGThe model bodies tested at Mach number 7.32 were hemispheres, blunt cones, and spherical segments. The mass addition consisted of air ejected through porous forward surfaces of the models. The experimental data consisted of heat transfer measurements from which boundary layer transitions were deduced. The data verified various applicable boundary layer codes in the laminar and transitional flow regimes. Empirical heating rate data correlations were developed for the laminar and turbulent flow regimes
Heat transfer measurements on blunt spherical segment nose and cylindrical body and flight test of r...
Measurements of the local heat transfer and pressure distribution have been made on six 2-inch-diame...
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall...
A wind-tunnel investigation was made to determine heat-transfer distributions on three steel sphere-...
Boundary-layer-transition and heat-transfer measurements were obtained from flight tests of blunt an...
Surface heat-transfer rates and pressures were measured at hypersonic speeds on sharp cones at zero ...
Numerical solutions are presented for the flow over a spherically blunted cone and hyperboloid with ...
Measurements of aerodynamic heat transfer have been made at several stations on the 15 deg total-ang...
A highly polished hemisphere-cone having a ratio of nose radius to base radius of 0.74 and a half-an...
Tests at M = 8.2 show that a simulated rocket plume at the base of a blunted cone can cause large ar...
Heat transfer and boundary layer behavior in subsonic oscillating and steady airflow
Convective heat transfer and pressure distribution measurements on lifting blunt cone reentry bod
Effect of radiative heat transfer in low Reynolds number hypersonic flow about blunt bod
Measurement of convective heat transfer rates on conical nosecap and hemispherical afterbody configu...
Aerobraking has been proposed as an efficient means of decelerating spacecraft for planetary mission...
Heat transfer measurements on blunt spherical segment nose and cylindrical body and flight test of r...
Measurements of the local heat transfer and pressure distribution have been made on six 2-inch-diame...
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall...
A wind-tunnel investigation was made to determine heat-transfer distributions on three steel sphere-...
Boundary-layer-transition and heat-transfer measurements were obtained from flight tests of blunt an...
Surface heat-transfer rates and pressures were measured at hypersonic speeds on sharp cones at zero ...
Numerical solutions are presented for the flow over a spherically blunted cone and hyperboloid with ...
Measurements of aerodynamic heat transfer have been made at several stations on the 15 deg total-ang...
A highly polished hemisphere-cone having a ratio of nose radius to base radius of 0.74 and a half-an...
Tests at M = 8.2 show that a simulated rocket plume at the base of a blunted cone can cause large ar...
Heat transfer and boundary layer behavior in subsonic oscillating and steady airflow
Convective heat transfer and pressure distribution measurements on lifting blunt cone reentry bod
Effect of radiative heat transfer in low Reynolds number hypersonic flow about blunt bod
Measurement of convective heat transfer rates on conical nosecap and hemispherical afterbody configu...
Aerobraking has been proposed as an efficient means of decelerating spacecraft for planetary mission...
Heat transfer measurements on blunt spherical segment nose and cylindrical body and flight test of r...
Measurements of the local heat transfer and pressure distribution have been made on six 2-inch-diame...
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall...