Add to ORKGA new type of sensor with the flexible substrate is introduced. It is applicable in measuring instantaneous heat flux on the model surface in a hypersonic shock tunnel. The working principle, structure and manufacture process of the sensor are presented. The substrate thickness and the dynamic response parameter of the sensor are calculated. Because this sensor was successfully used in measuring the instantaneous heat flux on the surface of a flat plate in a detonation-driven shock tunnel, it may be effective in measuring instantaneous heat flux on the model surface
A small heat transfer probe, operating in the free molecule tow regime, was developed with the purpo...
Reflected shock tunnels can reproduce realistic pressures, speeds, and temperatures of atmospheric h...
An electrical preheating technique applied to a carbon-based model in an impulse facility h...
Abstract To measure heat flux on the sharp leading edge and other surface with very small curvature ...
Two methods for calculating surface heat transfer rates from sub-surface temperature measurements ar...
A fast response temperature probe which may be used for a method for measuring an instantaneous temp...
This work seeks to apply the novel heat flux sensor called as the Atomic Layer Thermopile to measure...
A microcontroller-based data acquisition system has been developed for use in the T-ADFA hypersonic ...
A fast-response total temperature probe relying on transient heat flux measurements at different sur...
Robust fast-response transient calorimeters with novel calorimeter elements have attracted the atten...
The aerodynamic environment in the test section of a hypersonic shock tunnel is very hostile as the ...
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center DLR) is one of the ma...
This thesis is concerned with the development of a method to measure the temperature of a metal surf...
Already, aerospace engineers have to deal with the effects of hypersonic flow: intercontinental rock...
A new variant of MEMS surface fence is proposed for shear-stress estimation under high-speed, high-t...
A small heat transfer probe, operating in the free molecule tow regime, was developed with the purpo...
Reflected shock tunnels can reproduce realistic pressures, speeds, and temperatures of atmospheric h...
An electrical preheating technique applied to a carbon-based model in an impulse facility h...
Abstract To measure heat flux on the sharp leading edge and other surface with very small curvature ...
Two methods for calculating surface heat transfer rates from sub-surface temperature measurements ar...
A fast response temperature probe which may be used for a method for measuring an instantaneous temp...
This work seeks to apply the novel heat flux sensor called as the Atomic Layer Thermopile to measure...
A microcontroller-based data acquisition system has been developed for use in the T-ADFA hypersonic ...
A fast-response total temperature probe relying on transient heat flux measurements at different sur...
Robust fast-response transient calorimeters with novel calorimeter elements have attracted the atten...
The aerodynamic environment in the test section of a hypersonic shock tunnel is very hostile as the ...
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center DLR) is one of the ma...
This thesis is concerned with the development of a method to measure the temperature of a metal surf...
Already, aerospace engineers have to deal with the effects of hypersonic flow: intercontinental rock...
A new variant of MEMS surface fence is proposed for shear-stress estimation under high-speed, high-t...
A small heat transfer probe, operating in the free molecule tow regime, was developed with the purpo...
Reflected shock tunnels can reproduce realistic pressures, speeds, and temperatures of atmospheric h...
An electrical preheating technique applied to a carbon-based model in an impulse facility h...