Kießling, F. and Potkanski, W. (1) (1994) Nonlinear Flutter Analysis by a Continuation Method. 2nd International Conference Engineering Aero-Hydroelasticity EAHE, Pilsen, Czech Republic, June 6-10, 1994.
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Abstract
The application of a continuation method to the solution of a system of nonlinear flutter equations is presented. For practical analysis of complete aircraft a modal reduction is proposed, which is based on normal modes of the structure with all concentrated nonlinearities replaced by linear springs. In the solution process the stiffness matrix is modified by proper values resulting from harmonic balance. Results are given for a two-degree-of-freedom airfoil with nonlinear pitch stiffness and for a sailplane with several nonlinearities in the control system.
Item URL in elib: | https://elib.dlr.de/39698/ | |||||||||
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Document Type: | Conference or Workshop Item (Paper) | |||||||||
Additional Information: | LIDO-Berichtsjahr=1994, pages=6, | |||||||||
Title: | Nonlinear Flutter Analysis by a Continuation Method. | |||||||||
Authors: |
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Date: | 1994 | |||||||||
Open Access: | No | |||||||||
Gold Open Access: | No | |||||||||
In SCOPUS: | No | |||||||||
In ISI Web of Science: | No | |||||||||
Status: | Published | |||||||||
Keywords: | Nonlinear Vibration, Aeroelasticity, Continuation Methods, Harmonic Balance | |||||||||
Event Title: | 2nd International Conference Engineering Aero-Hydroelasticity EAHE, Pilsen, Czech Republic, June 6-10, 1994 | |||||||||
HGF - Research field: | UNSPECIFIED | |||||||||
HGF - Program: | Aeronautics | |||||||||
HGF - Program Themes: | other | |||||||||
DLR - Research area: | UNSPECIFIED | |||||||||
DLR - Program: | L ST - Starrflüglertechnologien | |||||||||
DLR - Research theme (Project): | UNSPECIFIED | |||||||||
Location: | Göttingen | |||||||||
Institutes and Institutions: | Institute of Aeroelasticity | |||||||||
Deposited By: | DLR-Beauftragter, elib | |||||||||
Deposited On: | 02 Apr 2006 | |||||||||
Last Modified: | 27 Apr 2009 10:51 |
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