In an investigation described in NACA Technical Report 110, it was shown that under certain conditions, particularly for the relatively low-speed flight of airships, the data obtained were not sufficiently accurate. This report describes an investigation in which the data obtained were sufficiently accurate and complete to enable the viscosity correction to be deduced quantitatively for a number of the air-speed pressure nozzles in common use. The report opens with a discussion of the theory of the performance of air-speed nozzles and of the calibration of the indicators, from which the theory of the altitude correction is developed. Then follows the determination of the performance characteristics of the nozzles and calibration constants u...
A NACA 64A010 pressure-instrumented airfoil was tested at transonic speeds over a range of angle of ...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
The study of circular-to-rectangular transition duct flows with and without inlet swirl is presented...
In an investigation described in NACA Technical Report 110, it was shown that under certain conditio...
Detailed unsteady boundary layer measurements are presented for eight airfoils oscillated in pitch t...
Report describes the development of a suitable speed nozzle for the first few thousand airplanes mad...
This report is section VIII of a series of reports on aeronautic instruments. The preceding reports ...
Herein is presented the collected data for tests in which a NACA 23012A aerofoil was subjected to a ...
A simple, airborne, flight-management descent algorithm was developed and programmed into a small pr...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
This collection of data on airfoils has been made from the published reports of a number of the lead...
The hot-wire anemometer suggests itself as a promising method for measuring the fluctuating air velo...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...
Herein is presented the collected data for tests in which an AHAVAW aerofoil was subjected to a vari...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
A NACA 64A010 pressure-instrumented airfoil was tested at transonic speeds over a range of angle of ...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
The study of circular-to-rectangular transition duct flows with and without inlet swirl is presented...
In an investigation described in NACA Technical Report 110, it was shown that under certain conditio...
Detailed unsteady boundary layer measurements are presented for eight airfoils oscillated in pitch t...
Report describes the development of a suitable speed nozzle for the first few thousand airplanes mad...
This report is section VIII of a series of reports on aeronautic instruments. The preceding reports ...
Herein is presented the collected data for tests in which a NACA 23012A aerofoil was subjected to a ...
A simple, airborne, flight-management descent algorithm was developed and programmed into a small pr...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
This collection of data on airfoils has been made from the published reports of a number of the lead...
The hot-wire anemometer suggests itself as a promising method for measuring the fluctuating air velo...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...
Herein is presented the collected data for tests in which an AHAVAW aerofoil was subjected to a vari...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
A NACA 64A010 pressure-instrumented airfoil was tested at transonic speeds over a range of angle of ...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
The study of circular-to-rectangular transition duct flows with and without inlet swirl is presented...