A technique was developed for measuring steady state heat transfer on a hemisphere cylinder and the results are compared with theory. The instrumentation consisted of a miniaturized thermopile of silver-constantan thermocouples approximately 1/8" x 1/16" x 1/100". The repeatability of readings with this device was found to be excellent. These heat measuring devices, or heat meters, were installed in both a ceramic hemisphere cylinder and in a similar metal one. There were obtained three different heat flow rates at each of six different combinations of tunnel pressure and temperature. The results compared very well with a theory developed by Lester Lees based upon the assumption of local similarity
A program to investigate the aerodynamic heat transfer of a nonisothermal hemisphere-cylinder has be...
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle coni...
A method for recording the local heat-transfer coefficients on bodies in flow was developed. The cyl...
A technique was developed for measuring steady state heat transfer on a hemisphere cylinder and the ...
An experimental investigation was made in the GALCIT hypersonic wind tunnel, leg number 1, at a nomi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Aerodynamic heat transfer measurements on low fineness ratio cylinder at free stream Mach number of ...
The knowledge of air temperature has always been an. essential part of any flight test records for ...
A steady-state technique of heat-transfer measurement has been developed based on the method of Seba...
Instrumentation technique for simple or complicated shapes for measuring aerodynamic heat transfer i...
Abstract: Equilibrium temperatures and heat-transfer coefficients for a hemispherical nose have been...
The objectives of this program are to develop heat flux sensors suitable for installation in hot sec...
An irmestigaticm to determine and correlate ihe experi-mental mmface heai-transjer coefitienis of ji...
"An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation ...
The successful design of a long-lived and efficient gas turbine engine requires a good knowledge of ...
A program to investigate the aerodynamic heat transfer of a nonisothermal hemisphere-cylinder has be...
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle coni...
A method for recording the local heat-transfer coefficients on bodies in flow was developed. The cyl...
A technique was developed for measuring steady state heat transfer on a hemisphere cylinder and the ...
An experimental investigation was made in the GALCIT hypersonic wind tunnel, leg number 1, at a nomi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Aerodynamic heat transfer measurements on low fineness ratio cylinder at free stream Mach number of ...
The knowledge of air temperature has always been an. essential part of any flight test records for ...
A steady-state technique of heat-transfer measurement has been developed based on the method of Seba...
Instrumentation technique for simple or complicated shapes for measuring aerodynamic heat transfer i...
Abstract: Equilibrium temperatures and heat-transfer coefficients for a hemispherical nose have been...
The objectives of this program are to develop heat flux sensors suitable for installation in hot sec...
An irmestigaticm to determine and correlate ihe experi-mental mmface heai-transjer coefitienis of ji...
"An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation ...
The successful design of a long-lived and efficient gas turbine engine requires a good knowledge of ...
A program to investigate the aerodynamic heat transfer of a nonisothermal hemisphere-cylinder has be...
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle coni...
A method for recording the local heat-transfer coefficients on bodies in flow was developed. The cyl...