Parametric combination resonance instability characteristics of laminated composite curved panels with circular cutout subjected to non-uniform loading with damping-Reference-Cited by-同舟云学术

Parametric combination resonance instability characteristics of laminated composite curved panels with circular cutout subjected to non-uniform loading with damping

Published:2007-03 Issue:3 Volume:49 Page:317-334
ISSN:0020-7403
Container-title:International Journal of Mechanical Sciences
language:en
Short-container-title:International Journal of Mechanical Sciences

Author:

Udar Ratnakar Shankarrao,Datta Prosun Kumar

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference51 articles.

1. The dynamic stability of elastic systems;Bolotin,1964

2. On parametric response of structures;Evan-Iwanowski;Applied Mechanics Review,1965

3. Large amplitude flexural vibration of layered composite plates with cutout;Reddy;Journal of Sound and Vibration,1982

4. Free vibration of composite rectangular plates with rectangular cutouts;Lee;Computers and Structures,1987

5. Buckling behavior of compression loaded symmetrically laminated angle-ply plates with holes;Nemeth;American Institute of Aeronautics and Astronautics Journal,1988

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