Reynolds number dependence of Apollo near-wake temperature.
Reynolds number dependence of near wake temperature of reentering probes and spacecraft determined using Apollo model temperature surveys for stagnation pressures
Huber, P. W.↗
Engineering topics
Hunt, J. L.
Publications and source records attributed to Hunt, J. L..
Experimental flow field and heat-transfer investigation of several tension shell configurations at a Mach number of 8
Flow field, pressure distributions, and heat transfer distribution of several tension shell configurations at hypersonic speeds
HEAT TRANSFER↗
Comment on ''measurement of aerodynamic heating of wind-tunnel models by means of temperature- sensitive paint.''
Measuring aerodynamic heating of wind-tunnel models by temperature sensitive paint, noting ambient pressure effect
TEMPERATURE INDICATOR↗
Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data
Fusible thin film coatings used in determining aerodynamic heat transfer coefficients at hypersonic speeds
THIN FILM↗
An improved technique for obtaining quantitative aerodynamic heat-transfer data with surface coating materials.
Phase change photographs used for quantitative aerodynamic heat transfer data with surface coating materials
COATING↗