Add to ORKGSome experimental heating data on concave and convex hemispherical nose shapes and hemispherical depressions on a blunted 30 ' cone have been obtained. Data obtained at Mach numbers up to approximately 8.5 indicate that the heating of the stagnation point of a concave hemi-spherical nose shape is approximately one-third that of a convex hemi-spherical nose shape at a Mach number of 2 and approximately one-tenth that of a convex hemispherical nose shape at a Mach number of 8
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle coni...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Comparisons of the development of flow over a cylinder with a 20° cone nose and a cylinder with an o...
Results are presented from recent investigations of the aeroaynamic heating rates of blunt nose shap...
Results are presented from investigations of the aerodynamic heating rates of blunt nose shapes at M...
Skin temperatures and surface pressures have been measured a t a number of locations on a s l igh t ...
Hypersonic flight is one of the most important transportations in the future and it refers to the fl...
Pressure and heat-transfer measurements of flat face of blunted 10 deg half-cone body or semidisk at...
Skin-temperature measurements have been made at several locations on a flat-faced cone-cylinder nose...
Aerodynamic-heating data were obtained on the conical nose of model 2 between Mach numbers 1.1 to 4....
Abstract: Equilibrium temperatures and heat-transfer coefficients for a hemispherical nose have been...
Measurement of convective heat transfer rates on conical nosecap and hemispherical afterbody configu...
The present work numerically and experimentally investigates Mach 5.8 flow past passively modified n...
Hypersonic vehicles are exposed to severe heating loads during their flight in the atmosphere. In or...
Effects of controlled heat addition into the high temperature, chemically reacting shock layer of a ...
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle coni...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Comparisons of the development of flow over a cylinder with a 20° cone nose and a cylinder with an o...
Results are presented from recent investigations of the aeroaynamic heating rates of blunt nose shap...
Results are presented from investigations of the aerodynamic heating rates of blunt nose shapes at M...
Skin temperatures and surface pressures have been measured a t a number of locations on a s l igh t ...
Hypersonic flight is one of the most important transportations in the future and it refers to the fl...
Pressure and heat-transfer measurements of flat face of blunted 10 deg half-cone body or semidisk at...
Skin-temperature measurements have been made at several locations on a flat-faced cone-cylinder nose...
Aerodynamic-heating data were obtained on the conical nose of model 2 between Mach numbers 1.1 to 4....
Abstract: Equilibrium temperatures and heat-transfer coefficients for a hemispherical nose have been...
Measurement of convective heat transfer rates on conical nosecap and hemispherical afterbody configu...
The present work numerically and experimentally investigates Mach 5.8 flow past passively modified n...
Hypersonic vehicles are exposed to severe heating loads during their flight in the atmosphere. In or...
Effects of controlled heat addition into the high temperature, chemically reacting shock layer of a ...
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle coni...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Comparisons of the development of flow over a cylinder with a 20° cone nose and a cylinder with an o...