A thin film device was designed and fabricated to measure surface temperatures. An array of eight integrated thermal sensors are mounted on a 0.002 inch (0.05 mm) Kapton film and multiplexed to obtain an area thermal measurement. The device was tested on a flat plate airfoil and demonstrated a temperature variation of 0.55 C maximum and 0.05 C minimum compared to embedded thermocouples. Future improvements are also discussed
Bonding, density, and thickness of coatings have a vital effect on their performance in many applica...
This research is motivated by two observations: No report has been found so far in studies of water...
Low and ultra low temperature cryogenic cooler systems for future space missions include mechanical,...
Programs to develop research instrumentation for use in turbine engine hot sections are described. T...
Two methods were used to calculate the heat flux to full-coverage film cooled airfoils and, subseque...
Ball bearing endurance tests and lubricant film thickness measurements under conditions of high temp...
Thermal energy storage (TES) enables a solar dynamic system to deliver constant electric power throu...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...
Results of preliminary tests to measure ice growth on an airfoil during flight icing conditions are ...
The Lewis Research Center gas turbine Hot Section Test Facility was developed to provide a real engi...
Heat transfer across metal surfaces under transient temperature and pressure environmen
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...
Radiosonde temperature measurements are subject to errors, not the least of which is the effect of l...
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
This report describes the results of a small study program in support of the design studies for NASA...
Bonding, density, and thickness of coatings have a vital effect on their performance in many applica...
This research is motivated by two observations: No report has been found so far in studies of water...
Low and ultra low temperature cryogenic cooler systems for future space missions include mechanical,...
Programs to develop research instrumentation for use in turbine engine hot sections are described. T...
Two methods were used to calculate the heat flux to full-coverage film cooled airfoils and, subseque...
Ball bearing endurance tests and lubricant film thickness measurements under conditions of high temp...
Thermal energy storage (TES) enables a solar dynamic system to deliver constant electric power throu...
An analytical model for calculation of ascent steady state tile loading was developed and validated ...
Results of preliminary tests to measure ice growth on an airfoil during flight icing conditions are ...
The Lewis Research Center gas turbine Hot Section Test Facility was developed to provide a real engi...
Heat transfer across metal surfaces under transient temperature and pressure environmen
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...
Radiosonde temperature measurements are subject to errors, not the least of which is the effect of l...
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
This report describes the results of a small study program in support of the design studies for NASA...
Bonding, density, and thickness of coatings have a vital effect on their performance in many applica...
This research is motivated by two observations: No report has been found so far in studies of water...
Low and ultra low temperature cryogenic cooler systems for future space missions include mechanical,...