Add to ORKGA method is described for checking a correction formula, based partly on theoretical considerations, for adiabatic compression and friction in flight tests and determining the value of the constant. It is necessary to apply a threefold correction to each thermometer reading. They are a correction for adiabatic compression, friction and for time lag
The value of the transmission function in a heterogeneous atmosphere is determined by iterative corr...
In an investigation described in NACA Technical Report 110, it was shown that under certain conditio...
In this report is described an experimental method which the writer has evolved for dealing with air...
A method is described for checking a correction formula, based partly on theoretical considerations,...
Subsonic wind tunnel calibration of Arcasonde 1-A atmospheric temperature sensing unit at simulated ...
Measurements of temperature variations in the atmosphere near the tropopause over land in the vicini...
A method for calculating the rate of heat transfer from the surface of an airfoil or streamline body...
High temperature, high altitude total temperature sensor development - thermocouple devic
Errors that occur in conventional measurement instruments connected to a pitot-static system affect ...
The hot-wire anemometer suggests itself as a promising method for measuring the fluctuating air velo...
A temperature measurement system, which allows the simultaneous sampling of up to 80 separate thermo...
The knowledge of air temperature has always been an. essential part of any flight test records for ...
The sources of error that may enter into the measurement of airspeed by pitot-static methods are rev...
The applicability of the self-heating technique for checking the calibration of platinum resistance ...
A method is described of calibrating airspeed installations on airplanes at transonic and supersonic...
The value of the transmission function in a heterogeneous atmosphere is determined by iterative corr...
In an investigation described in NACA Technical Report 110, it was shown that under certain conditio...
In this report is described an experimental method which the writer has evolved for dealing with air...
A method is described for checking a correction formula, based partly on theoretical considerations,...
Subsonic wind tunnel calibration of Arcasonde 1-A atmospheric temperature sensing unit at simulated ...
Measurements of temperature variations in the atmosphere near the tropopause over land in the vicini...
A method for calculating the rate of heat transfer from the surface of an airfoil or streamline body...
High temperature, high altitude total temperature sensor development - thermocouple devic
Errors that occur in conventional measurement instruments connected to a pitot-static system affect ...
The hot-wire anemometer suggests itself as a promising method for measuring the fluctuating air velo...
A temperature measurement system, which allows the simultaneous sampling of up to 80 separate thermo...
The knowledge of air temperature has always been an. essential part of any flight test records for ...
The sources of error that may enter into the measurement of airspeed by pitot-static methods are rev...
The applicability of the self-heating technique for checking the calibration of platinum resistance ...
A method is described of calibrating airspeed installations on airplanes at transonic and supersonic...
The value of the transmission function in a heterogeneous atmosphere is determined by iterative corr...
In an investigation described in NACA Technical Report 110, it was shown that under certain conditio...
In this report is described an experimental method which the writer has evolved for dealing with air...