Finite-element analysis of the fluttering panels excited by external forces

Journal of Sound and Vibration

Volumn 224, Issue 5, 1999, Pages 917-935

  Surace, G ^a   Udrescu, R ^b  

^a POLITECNICO DI TORINO   (Italy)

^b National Research and Development Institute for Gas Turbines COMOTI   (Romania)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0039628154     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1999.2223     Document Type: Article

References (22)

1. E. H. DOWELL and M. ILGAMOV 1988 Studies in Nonlinear Aeroelasticity. Berlin: Springer.
2. R. L. BISPLINGHOFF and H. ASHLEY 1962 Principles of Aeroelasticity. New York: Wiley.
3. R. BACKER 1992 Plenary Session 8 AIAA Dynamics Specialists Conference, Dallas. F-117A structures and dynamics design.
4. E. H. DOWELL 1970 AIAA Journal 8, 385-399. Panel flutter: a review of the aeroelastic stability of plates and shells.
5. M. D. OLSON 1970 AIAA Journal 8, 747-752. Some flutter solutions using finite elements.
6. C. MEI 1977 AIAA Journal 15, 1107-1110. A finite element approach for nonlinear panel flutter.
7. C. E. GRAY, C. MEI and C. P. SHORE 1991 AIAA Journal 29, 290-298. Finite-element method for large-amplitude two-dimensional panel flutter at hypersonic speeds.
8. C. MEI and H. C. WANG 1982 Proceedings of the International Conference on Finite Element Method, Shanghai, China, New York: Gordon & Breach, 944-951. Finite element analysis of large amplitude supersonic flutter of panels.
9. A. D. HAN and T. Y. YANG 1983 AIAA Journal 21, 1453-1461. Nonlinear panel flutter using high-order triangular finite elements.
10. J. C. HOUBOLT 1958 Ph.D. Thesis Eidenössischen Technichen Hochschule, Swiss Federal Inst. of Technology, Zürich, Switzerland. A study of several aerothermoelastic problems of aircraft structures in high-speed flight.
11. D. Y. XUE and C. MEI 1993 AIAA Journal 31, 154-162. Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow.
12. R. I. DIXON and C. MEI 1993 AIAA Journal 31, 701-707. Finite element analysis of large-amplitude panel flutter of thin laminates.
13. R. C. ZHOU, Y. XUE and C. MEI 1994 AIAA Journal 32, 2044-2052. Finite element time domain-modal formulation for nonlinear flutter of composite panels.
14. Z. LAI, D. XUE, J-K. HUANG and C. MEI 1995 Journal of Intelligent Material Systems and Structures 6, 274-282. Panel flutter limit-cycle suppression with piezoelectric actuation.
15. R. C. ZHOU, Z. LAI, D. XUE, J-K. HUANG and C. MEI 1995 AIAA Journal 33, 1098-1105. Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method.
16. R. C. ZHOU, C. MEI and J-K. HUANG 1996 AIAA Journal 34, 347-357. Suppression of nonlinear panel flutter at supersonic speeds and elevated temperatures.
17. E. H. DOWELL 1974 Aeroelasticity of Plates and Shells. Dordrecht: Kluwer Academic Publishers.
18. J. A. BAILIE and J. E. MCFEELY 1968 AIAA Journal 6, 332-337. Panel flutter in hypersonic flow.
19. R. UDRESCU 1998 A Collection of Technical Papers of the 39th AIAA/ASME/ ASCE/AHS/ACS Structures, Structural Dynamics and Materials Conference 2, 1252-1262, AIAA paper #98-1843. A higher finite element model in nonlinear panel flutter analysis.
20. J. ARGYRIS and H. P. MLEJNEK 1986-1988 Die Metode der Finiten Elementen (3 vols.). Braunschweig/Wiesbaden.
21. J. ARGYRIS and R. UDRESCU 1993 Technical Report, Institute for Computer Applications, University of Stuttgart. Nonlinear panel flutter on high-order FE model-natural approach.
22. R. UDRESCU 1996 Ph.D. Dissertation, Aerospace Department, "Politehnica" University of Bucharest. Contributions to the aeroelasticity of panels modeled by high-order finite elements (in Romanian).