Experimental heat flux measurements are made using both thermocouple and thin film gages in high-temperature, hypersonic flows. Thermocouple and thin film gages have individually been extensively used in relatively high and low enthalpy conditions respectively. In this study, three test conditions with varying (intermediate) stagnation enthalpies, Mach and Reynolds numbers are created in an expansion tube facility, and temperature histories and heat flux measurements obtained using the two gage types are directly compared. Gage performance in terms of survivability, response, uncertainty, and signal-to-noise ratio is assessed for both blunt body and flat plate models
Aerodynamic heating in hypersonic space vehicles is an important factor to be considered in their de...
Fast response heat flux gauges relying on the semi-infinite heat conduction principle have commonly ...
Fast response heat flux gauges relying on the semi-infinite heat conduction principle have commonly ...
Reliable prediction of the high heat transfer rates experienced during the hypersonic portion of pl...
Reliable prediction of the high heat transfer rates experienced during the hypersonic portion of pl...
Thin film gages deposited at the stagnation region of small (8.1-mm-diameter) hemispheres and gages ...
Prediction of heat transfer is integral to development of hypersonic vehicles. Underprediction of he...
Prediction of heat transfer is integral to development of hypersonic vehicles. Underprediction of he...
A new form of surface junction thermocouple sensor has been developed and tested. The novel feature ...
The aerodynamic environment in the test section of a hypersonic shock tunnel is very hostile as the ...
A special thin film-hardware material thermocouple (TC) and heat flux gauge concept for a reasonably...
A new thin-film heat flux gage has been fabricated specifically for severe high temperature operatio...
The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat...
Data on surface heat flux is critical in all hypersonic missions due to the extent of risk and the p...
It is necessary to use high response instrumentation in hypervelocity test facilities. High response...
Aerodynamic heating in hypersonic space vehicles is an important factor to be considered in their de...
Fast response heat flux gauges relying on the semi-infinite heat conduction principle have commonly ...
Fast response heat flux gauges relying on the semi-infinite heat conduction principle have commonly ...
Reliable prediction of the high heat transfer rates experienced during the hypersonic portion of pl...
Reliable prediction of the high heat transfer rates experienced during the hypersonic portion of pl...
Thin film gages deposited at the stagnation region of small (8.1-mm-diameter) hemispheres and gages ...
Prediction of heat transfer is integral to development of hypersonic vehicles. Underprediction of he...
Prediction of heat transfer is integral to development of hypersonic vehicles. Underprediction of he...
A new form of surface junction thermocouple sensor has been developed and tested. The novel feature ...
The aerodynamic environment in the test section of a hypersonic shock tunnel is very hostile as the ...
A special thin film-hardware material thermocouple (TC) and heat flux gauge concept for a reasonably...
A new thin-film heat flux gage has been fabricated specifically for severe high temperature operatio...
The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat...
Data on surface heat flux is critical in all hypersonic missions due to the extent of risk and the p...
It is necessary to use high response instrumentation in hypervelocity test facilities. High response...
Aerodynamic heating in hypersonic space vehicles is an important factor to be considered in their de...
Fast response heat flux gauges relying on the semi-infinite heat conduction principle have commonly ...
Fast response heat flux gauges relying on the semi-infinite heat conduction principle have commonly ...