Add to ORKGTo fully characterize advanced high temperature heat flux sensors, calibration and testing is required at full engine temperature. This required the development of unique high temperature heat flux test facilities. These facilities were developed, are in place, and are being used for advanced heat flux sensor development
The work described is part of a program (Englund and Seasholtz, 1988) to develop sensors and sensing...
Tasks performed in this project were defined in a September 9, 1994 meeting of representatives of Va...
The objective is to describe continuing efforts to develop methods for measuring surface heat flux, ...
A two-phase program is conducted to develop heat flux sensors capable of making heat flux measuremen...
Various configurations of high temperature, heat flux sensors were studied to determine their suitab...
The measurement of high temperatures and the influence of heat transfer data is not strictly a probl...
A new automated, computer controlled heat flux measurement facility is described. Continuous transie...
Programs to develop research instrumentation for use on hot section components of turbine engines ar...
The objectives of this program are to develop heat flux sensors suitable for installation in hot sec...
Comparative heat flux measurements were performed in the hypersonic high enthalpy flow field of the ...
A new thin-film heat flux gage has been fabricated specifically for severe high temperature operatio...
The development of heat flux sensors for gas turbine blades and vanes and the demonstration of heat ...
Comparative heat flux measurements were performed in the hypersonic high enthalpy flow field of the ...
To monitor the high-intensity heat flux conditions that occur in the space shuttle main engine (SSME...
There is a need to more thoroughly characterize the hostile space shuttle main engine (SSME) turbopu...
The work described is part of a program (Englund and Seasholtz, 1988) to develop sensors and sensing...
Tasks performed in this project were defined in a September 9, 1994 meeting of representatives of Va...
The objective is to describe continuing efforts to develop methods for measuring surface heat flux, ...
A two-phase program is conducted to develop heat flux sensors capable of making heat flux measuremen...
Various configurations of high temperature, heat flux sensors were studied to determine their suitab...
The measurement of high temperatures and the influence of heat transfer data is not strictly a probl...
A new automated, computer controlled heat flux measurement facility is described. Continuous transie...
Programs to develop research instrumentation for use on hot section components of turbine engines ar...
The objectives of this program are to develop heat flux sensors suitable for installation in hot sec...
Comparative heat flux measurements were performed in the hypersonic high enthalpy flow field of the ...
A new thin-film heat flux gage has been fabricated specifically for severe high temperature operatio...
The development of heat flux sensors for gas turbine blades and vanes and the demonstration of heat ...
Comparative heat flux measurements were performed in the hypersonic high enthalpy flow field of the ...
To monitor the high-intensity heat flux conditions that occur in the space shuttle main engine (SSME...
There is a need to more thoroughly characterize the hostile space shuttle main engine (SSME) turbopu...
The work described is part of a program (Englund and Seasholtz, 1988) to develop sensors and sensing...
Tasks performed in this project were defined in a September 9, 1994 meeting of representatives of Va...
The objective is to describe continuing efforts to develop methods for measuring surface heat flux, ...