Exploratory work is in progress to apply thin-film thermocouples to localized heat transfer measurements on turbine engine vanes and blades. The emerging thin-film thermocouple technology shows great potential to improve the accuracy of local heat transfer measurements. To verify and master the experimental methodology of thin-film thermocouples, the NASA Lewis Research Center conducted a proof-of-concept experiment in a controlled environment before applying the thin-film sensors to turbine tests
This thesis describes the development of heated double-sided thin film gauge configurations for tran...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
Paper presented at the 12. Symp. on Measuring Techniques for Transonic and Supersonic Flow in Cascad...
The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
The objective is to develop thin-film thermocouples for Space Shuttle Main Engine (SSME) components....
The objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
Hot section temperatures in gas turbine engines can reach 1500°C, an environment in which implementi...
Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied t...
The Space Shuttle Main Engine (SSME) turbine environment stresses engine components to their design ...
This thesis describes the development of heated double-sided thin film gauge configurations for tran...
The paper describes application of two modern experimental techniques, thin-film thermocouples and p...
Advanced thin film sensors that can provide accurate surface temperature, strain, and heat flux meas...
This paper describes the development of heated double-sided thin film gauge configurations for trans...
This thesis describes the development of heated double-sided thin film gauge configurations for tran...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
Paper presented at the 12. Symp. on Measuring Techniques for Transonic and Supersonic Flow in Cascad...
The paper describes a proof-of-concept experiment on thin-film thermocouples used for localized heat...
As a demonstration of technology maturation, a thin-film temperature sensor probe was fabricated and...
Thin film thermocouples provide a minimally intrusive means of measuring surface temperature in host...
The objective is to develop thin-film thermocouples for Space Shuttle Main Engine (SSME) components....
The objective is to develop thin film thermocouples (TFTC) for Space Shuttle Main Engine (SSME) comp...
Hot section temperatures in gas turbine engines can reach 1500°C, an environment in which implementi...
Prototype thin film heat flux sensors have been constructed and tested. The sensors can be applied t...
The Space Shuttle Main Engine (SSME) turbine environment stresses engine components to their design ...
This thesis describes the development of heated double-sided thin film gauge configurations for tran...
The paper describes application of two modern experimental techniques, thin-film thermocouples and p...
Advanced thin film sensors that can provide accurate surface temperature, strain, and heat flux meas...
This paper describes the development of heated double-sided thin film gauge configurations for trans...
This thesis describes the development of heated double-sided thin film gauge configurations for tran...
Temperatures of hot section components in today’s gas turbine engines reach as high as 1,500 °C, mak...
Paper presented at the 12. Symp. on Measuring Techniques for Transonic and Supersonic Flow in Cascad...