The applicability of the self-heating technique for checking the calibration of platinum resistance thermometers located inside wind tunnels was investigated. This technique is based on a steady state measurement of resistance increase versus joule heating. This method was found to be undesirable, mainly because of the fluctuations of flow variables during any wind tunnel testing
An experimental method for direct measurement of the thermophysical properties of wind tunnel heat t...
Aerodynamic force measurements on a generalized 75 deg delta wing model with sharp leading edges wer...
Calibration of commercial platinum resistance thermometer using Z function interpolatio
The calibration and stability of four surface temperature measuring industrial platinum resistance t...
Thirty-one commercially designed platinum resistance thermometers were evaluated for applicability t...
Two methods were used to calculate the heat flux to full-coverage film cooled airfoils and, subseque...
Platinum resistance thermometers tested and evaluated in cryogenic temperature measuremen
The Lewis Research Center gas turbine Hot Section Test Facility was developed to provide a real engi...
The use of a photographic pyrometer for nonintrusive measurement of high temperature surfaces in a w...
An electronic system is described which measures the surface temperature of a small portion of the s...
Programs to develop research instrumentation for use in turbine engine hot sections are described. T...
A thin film device was designed and fabricated to measure surface temperatures. An array of eight in...
The thermal analysis of a heat exchanger for heating air to temperatures on the order of 3000 C for ...
A method is described for checking a correction formula, based partly on theoretical considerations,...
The hot-wire anemometer suggests itself as a promising method for measuring the fluctuating air velo...
An experimental method for direct measurement of the thermophysical properties of wind tunnel heat t...
Aerodynamic force measurements on a generalized 75 deg delta wing model with sharp leading edges wer...
Calibration of commercial platinum resistance thermometer using Z function interpolatio
The calibration and stability of four surface temperature measuring industrial platinum resistance t...
Thirty-one commercially designed platinum resistance thermometers were evaluated for applicability t...
Two methods were used to calculate the heat flux to full-coverage film cooled airfoils and, subseque...
Platinum resistance thermometers tested and evaluated in cryogenic temperature measuremen
The Lewis Research Center gas turbine Hot Section Test Facility was developed to provide a real engi...
The use of a photographic pyrometer for nonintrusive measurement of high temperature surfaces in a w...
An electronic system is described which measures the surface temperature of a small portion of the s...
Programs to develop research instrumentation for use in turbine engine hot sections are described. T...
A thin film device was designed and fabricated to measure surface temperatures. An array of eight in...
The thermal analysis of a heat exchanger for heating air to temperatures on the order of 3000 C for ...
A method is described for checking a correction formula, based partly on theoretical considerations,...
The hot-wire anemometer suggests itself as a promising method for measuring the fluctuating air velo...
An experimental method for direct measurement of the thermophysical properties of wind tunnel heat t...
Aerodynamic force measurements on a generalized 75 deg delta wing model with sharp leading edges wer...
Calibration of commercial platinum resistance thermometer using Z function interpolatio