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Aeroelasticity analysis of aircraft wings in flutter-onset or post-flutter regime

2007
Because the flutter phenomenon is usually associated with large deformations/deflections, the structural solution based on linear theory gives inaccurate or totally unphysical solution because the equilibrium of the structure is referred to the initial state of the structure.
B. Tian, K. N. Ghia
openaire   +1 more source

An Approximate Analysis of Nonlinear Flutter Problems

Journal of the Aerospace Sciences, 1959
The approximate analysis of nonlinear flutter problems by the method of KrylofT and BogoliubofT is outlined. The method is presented in a simple fashion based upon the concept of "harmonic balance." Because of the nature of the response of flutter systems to sinusoidal excitations of various frequencies, it appears that the method should be ...
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An online flutter analysis system

41st Structures, Structural Dynamics, and Materials Conference and Exhibit, 2000
W. Lo, C. Shih, C. Yan
openaire   +1 more source

Three-Dimensional Flutter Analysis

Journal of the Aeronautical Sciences (Institute of the Aeronautical Sciences), 1941
openaire   +1 more source

Vector Methods of Flutter Analysis

Journal of the Aeronautical Sciences, 1942
WILLIAM M. BLEAKNEY, J. DOUGLAS HAMM
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Complex Notation in Flutter Analysis

Journal of Structural Engineering, 1998
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Station Functions in Flutter Analysis

Journal of the Aeronautical Sciences, 1950
J. H. Greidanus, A. I. Van De Vooren
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