Add to ORKGInstrumentation technique for simple or complicated shapes for measuring aerodynamic heat transfer in hotshot tunne
Heat sensing instrument, using thermocouple junction connected under heavy conducting materia
An experimental method for direct measurement of the thermophysical properties of wind tunnel heat t...
A transient technique was used to measure heat transfer coefficients on stator airfoils in a high-te...
Thin film gages deposited at the stagnation region of small (8.1-mm-diameter) hemispheres and gages ...
A technique was developed for measuring steady state heat transfer on a hemisphere cylinder and the ...
Aerodynamic heat transfer measurements on low fineness ratio cylinder at free stream Mach number of ...
A technique is developed to measure the local convective heat transfer coefficient on a model surfac...
A technique is developed to measure the local convective heat transfer coefficient on a model surfac...
"An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation ...
Thermal performance and structural integrity are experimentally evaluated in the Langley 8-ft high t...
Free flight measurements of stagnation point convective heat transfer in air at hypersonic speed
Aerodynamic heating in hypersonic space vehicles is an important factor to be considered in their de...
In order to utilize the shock tube for quantitative investigations of some aerodynamic problems a th...
A facility for making heat transfer measurements on solid surfaces using transient techniques is con...
A new form of surface junction thermocouple sensor has been developed and tested. The novel feature ...
Heat sensing instrument, using thermocouple junction connected under heavy conducting materia
An experimental method for direct measurement of the thermophysical properties of wind tunnel heat t...
A transient technique was used to measure heat transfer coefficients on stator airfoils in a high-te...
Thin film gages deposited at the stagnation region of small (8.1-mm-diameter) hemispheres and gages ...
A technique was developed for measuring steady state heat transfer on a hemisphere cylinder and the ...
Aerodynamic heat transfer measurements on low fineness ratio cylinder at free stream Mach number of ...
A technique is developed to measure the local convective heat transfer coefficient on a model surfac...
A technique is developed to measure the local convective heat transfer coefficient on a model surfac...
"An experimental investigation was conducted at a test-section Mach number of 4.95 and a stagnation ...
Thermal performance and structural integrity are experimentally evaluated in the Langley 8-ft high t...
Free flight measurements of stagnation point convective heat transfer in air at hypersonic speed
Aerodynamic heating in hypersonic space vehicles is an important factor to be considered in their de...
In order to utilize the shock tube for quantitative investigations of some aerodynamic problems a th...
A facility for making heat transfer measurements on solid surfaces using transient techniques is con...
A new form of surface junction thermocouple sensor has been developed and tested. The novel feature ...
Heat sensing instrument, using thermocouple junction connected under heavy conducting materia
An experimental method for direct measurement of the thermophysical properties of wind tunnel heat t...
A transient technique was used to measure heat transfer coefficients on stator airfoils in a high-te...