A new trailing bomb-type instrument for photographically recording the flight-path angle and air speed of aircraft in unaccelerated flight is described. The instrument consists essentially of an inclinometer, air-speed meter and a film-drum case. The inclinometer carries an oil-damped pendulum which records optically the flight-path angle upon a rotating motor-driven film drum. The air-speed meter consists of a taut metal diaphragm of high natural frequency which is acted upon by the pressure difference of a Prandtl type Pitot-static tube. The inclinometer record and air-speed record are made optically on the same sensitive film. Two records taken by this instrument are shown
Commerical pilot eye scanning data previously collected were reanalyzed to evaluate how pilot used t...
A method is described for calibrating airspeed installation on airplanes at transonic and supersonic...
Aerodynamics data are obtained for the design of linked balancing tabs and effect of varied tab span...
A new trailing bomb-type instrument for photographically recording the flight-path angle and air spe...
N.A.C.A. has developed an instrument which makes a continuous record of the angular position of the ...
A new type of air speed meter is described which was designed by the technical staff of the National...
A new instrument is described which is capable of simultaneously recording the position of the three...
A method is described for synchronizing the different instrument records taken during flight testing...
This note contains photos and descriptions of airplane flight apparatus for use in conjunction with ...
A new instrument known as the NACA three component accelerometer is described in this note. This ins...
There are forwarded herewith the results of blade motion and bouncing tests on the Kellett KD-1 thre...
Part 1 contains a discussion and description of the various types of air speed measuring instruments...
The object of this report is the description of a method which seems to be practicable for determini...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
An air speed and attitude probe characterized by a pivot shaft normally projected from a data boom a...
Commerical pilot eye scanning data previously collected were reanalyzed to evaluate how pilot used t...
A method is described for calibrating airspeed installation on airplanes at transonic and supersonic...
Aerodynamics data are obtained for the design of linked balancing tabs and effect of varied tab span...
A new trailing bomb-type instrument for photographically recording the flight-path angle and air spe...
N.A.C.A. has developed an instrument which makes a continuous record of the angular position of the ...
A new type of air speed meter is described which was designed by the technical staff of the National...
A new instrument is described which is capable of simultaneously recording the position of the three...
A method is described for synchronizing the different instrument records taken during flight testing...
This note contains photos and descriptions of airplane flight apparatus for use in conjunction with ...
A new instrument known as the NACA three component accelerometer is described in this note. This ins...
There are forwarded herewith the results of blade motion and bouncing tests on the Kellett KD-1 thre...
Part 1 contains a discussion and description of the various types of air speed measuring instruments...
The object of this report is the description of a method which seems to be practicable for determini...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
An air speed and attitude probe characterized by a pivot shaft normally projected from a data boom a...
Commerical pilot eye scanning data previously collected were reanalyzed to evaluate how pilot used t...
A method is described for calibrating airspeed installation on airplanes at transonic and supersonic...
Aerodynamics data are obtained for the design of linked balancing tabs and effect of varied tab span...