Data, of interest to airplane designers, on flutter and vibration of structures to which control surfaces are attached; this source of danger may be controlled; modern methods of stress analyses and load factors in current use are adequate to provide all strength needed in airplane structures for flight in rough air, and for all necessary maneuvers. Before Int Automotive Eng Congress.
Airplane vibrations and flutter controllable by design
Soc Automotive Engrs J
Society of Automotive Engineers -- Journal ; 33 , n 3
1933
8 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Airplane Vibrations and Flutter Controllable by Design
SAE Technical Papers | 1933
|Airplane vibrations and flutter
Engineering Index Backfile | 1934
|Engineering Index Backfile | 1929
Flight flutter testing the B-58 airplane
NTRS | 1975
|Vibrations or flutter in airplanes
Engineering Index Backfile | 1944
|