This investigation was undertaken by the National Advisory Committee for Aeronautics for the purpose of increasing our knowledge on the behavior of the airplane during various maneuvers and to obtain values of the maximum angular velocities and accelerations in flight. The method consisted in flying a JN4H airplane through various maneuvers while records were being taken of the control position, the air speed, the angular velocity and the acceleration along the Z axis. The results showed that the maximum angular velocity about the X axis of radians per second in a barrel roll. The maximum angular acceleration about the X axis of -2.10 radians per (second) to the 2nd power occurred in a spin, while the maximum about the Y axis was 1.40 radians per (second) to the 2nd power when pulling suddenly out of a dive. These results have direct application to the design of airplane parts, such as propeller shaft and instruments.
A Study of Airplane Maneuvers with Special Reference to Angular Velocities
1923-01-01
Sonstige
Keine Angabe
Englisch
A study of airplane maneuvers with special reference to angular velocities
Engineering Index Backfile | 1922
|Notes on maximum airplane angular velocities
NTRS | 1943
|Notes on maximum airplane angular velocities
TIBKAT | 1943
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