The sources of error that may enter into the measurement of airspeed by pitot-static methods are reviewed in detail together with methods of flight calibration of airspeed installations. Special attention is given to the problem of accurate measurements of airspeed under conditions of high speed and maneuverability required of military airplanes. (author
This report presents the results of full-scale wind tunnel tests conducted to determine the ground-h...
Extensive experimental measurements have been made of the downwash angles and the wake characteristi...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
A method is described for calibrating airspeed installation on airplanes at transonic and supersonic...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
This collection of data on airfoils has been made from the published reports of a number of the lead...
Symbols and definition of various airspeed terms that have been adopted as standard by the NACA subc...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
Flight tests were made to determine the profile-drag coefficients of a portion of the original wing ...
The air forces on a systematic series of biplane and triplane cellule models are the subject of this...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
This report presents a concise survey of the measurement of air speed and ground speed on board airc...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
Statistical measurements of contact conditions have been obtained, by means of a special photographi...
This report presents the results of full-scale wind tunnel tests conducted to determine the ground-h...
Extensive experimental measurements have been made of the downwash angles and the wake characteristi...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
A method is described for calibrating airspeed installation on airplanes at transonic and supersonic...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
This collection of data on airfoils has been made from the published reports of a number of the lead...
Symbols and definition of various airspeed terms that have been adopted as standard by the NACA subc...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
Flight tests were made to determine the profile-drag coefficients of a portion of the original wing ...
The air forces on a systematic series of biplane and triplane cellule models are the subject of this...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
This report presents a concise survey of the measurement of air speed and ground speed on board airc...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
Statistical measurements of contact conditions have been obtained, by means of a special photographi...
This report presents the results of full-scale wind tunnel tests conducted to determine the ground-h...
Extensive experimental measurements have been made of the downwash angles and the wake characteristi...
In connection with the standardization of instruments used in the wind tunnel, this investigation wa...