Supersonic flutter analysis of stiffened laminated plates subject to thermal load

Journal of Sound and Vibration

Volumn 224, Issue 1, 1999, Pages 49-67

  Lee, I ^a   Lee, D M ^a   Oh, I K ^a  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0002209639     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1998.2113     Document Type: Article

References (19)

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3. E. H. DOWELL 1970 AIAA Journal 8, 385-399. Panel flutter: a review of the aeroelastic stability of plates and shells.
4. A. D HAN and T. Y. YANG 1983 AIAA Journal 21, 1453-1461 Nonlinear panel flutter using high order triangular finite elements.
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13. L. MORINO 1969 AIAA Journal 7, 405-410. A perturbation method for treating nonlinear panel flutter problems.
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17. D. M. LEE and I. LEE 1996 AIAA Journal 34, 637-639. Supersonic flutter analysis of stiffened isotropic and anisotropic panels.
18. D. M. LEE and I. LEE 1997 Composites & Structures 63, 371-378. Vibration behaviors of thermally postbuckled anisotropic plates using first-order shear deformable plate theory.
19. D. M. LEE and I. LEE 1995 Composites & Structures 57, 99-105. Vibration analysis of anisotropic plates with eccentric stiffeners.