Method described can be used to investigate possibility of flutter on such structures as airplane wings, tail surfaces, bomb doors, aircraft propeller blades, vehicular bridges, buildings, etc; with well known solution for air forces for two-dimensional flow over airfoil with aileron, equations were derived which can be used to determine flutter speed for wing or tail surfaces of any conventional airplane; use of still air vibration tests in obtaining structural friction of structures, and in checking part of flutter computations experimentally is indicated. (See also - discussion p 355-6)
General approach to flutter problem
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 49 , n 2
1941
11 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
General Approach to the FLUTTER PROBLEM
SAE Technical Papers | 1941
|Simple approach to wing flutter problem
Engineering Index Backfile | 1933
|Mechanism of flutter -- Theoretical and experimental investigation of flutter problem
Engineering Index Backfile | 1940
|An approach to the flutter problem in real fluids
TIBKAT | 1955
|A General Method for Flutter Optimization
AIAA | 1973
|