EFFECT OF CONTROL TRAILING-EDGE THICKNESS OR ASPECT RATIO ON THE OSCILLATING HINGE-MOMENT AND FLUTTER CHARACTERISTICS OF A FLAPTYPE CONTROL AT TRANSONIC SPEEDS

William C. Moseley,Robert F Thompson

EFFECT OF CONTROL TRAILING-EDGE THICKNESS OR ASPECT RATIO ON THE OSCILLATING HINGE-MOMENT AND FLUTTER CHARACTERISTICS OF A FLAPTYPE CONTROL AT TRANSONIC SPEEDS

1958

William C. Moseley
Robert F Thompson

Control trailing-edge thickness and aspect ratio effect on oscillating hinge-moment and flutter characteristics of flap-type controls. Results regarding damping moments and flutter characteristics and spring moments are provided.

Keywords:

Flutter
Oscillation
Flight control surfaces
Transonic
Aerospace engineering
Torque
Hinge
Physics
Trailing edge
Structural engineering

Correction
Source
Cite
Save
Machine Reading By IdeaReader

References

Citations