Nonlinear aeroelasticity
Publication
, Journal Article
Dowell, E; Edwards, J; Strganac, T
Published in: Journal of Aircraft
January 1, 2003
Substantial progress has been made in modeling and understanding nonlinear aeroelastic phenomena. Experimental and theoretical investigations have shown good correlation for a number of nonlinear physical mechanisms. A number of physical mechanisms can lead to nonlinear aeroelastic response including the impact of static fluid or static structural nonlinearities in changing the flutter boundary of an aeroelastic system. The good news is that finite amplitude oscillations can in some cases replace what would otherwise be the rapidly growing and destructive oscillations of classical flutter behavior.
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Published In
Journal of Aircraft
DOI
EISSN
1533-3868
ISSN
0021-8669
Publication Date
January 1, 2003
Volume
40
Issue
5
Start / End Page
857 / 874
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering
Citation
APA
Chicago
ICMJE
MLA
NLM
Dowell, E., Edwards, J., & Strganac, T. (2003). Nonlinear aeroelasticity. Journal of Aircraft, 40(5), 857–874. https://doi.org/10.2514/2.6876
Dowell, E., J. Edwards, and T. Strganac. “Nonlinear aeroelasticity.” Journal of Aircraft 40, no. 5 (January 1, 2003): 857–74. https://doi.org/10.2514/2.6876.
Dowell E, Edwards J, Strganac T. Nonlinear aeroelasticity. Journal of Aircraft. 2003 Jan 1;40(5):857–74.
Dowell, E., et al. “Nonlinear aeroelasticity.” Journal of Aircraft, vol. 40, no. 5, Jan. 2003, pp. 857–74. Scopus, doi:10.2514/2.6876.
Dowell E, Edwards J, Strganac T. Nonlinear aeroelasticity. Journal of Aircraft. 2003 Jan 1;40(5):857–874.
Published In
Journal of Aircraft
DOI
EISSN
1533-3868
ISSN
0021-8669
Publication Date
January 1, 2003
Volume
40
Issue
5
Start / End Page
857 / 874
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering