Inclusion of transverse shear deformation in exact buckling and vibration analysis of composite plate assemblies-Reference-Cited by-同舟云学术

Inclusion of transverse shear deformation in exact buckling and vibration analysis of composite plate assemblies

Published:1992-04-13 Issue: Volume: Page:
ISSN:
Container-title:33rd Structures, Structural Dynamics and Materials Conference
language:
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Author:

ANDERSON MELVIN¹,KENNEDY DAVID²

Affiliation:

1. Old Dominion University Research Foundation, Norfolk, VA

2. Cardiff, University College, Wales

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2287

Reference8 articles.

1. Acknowledgement- This work was supported by the National Aeronautics and Space Administration under grant NAS1-18584-05 and Coo erative Agreement NCCW-000002. The worI?of the second author was also sup orted by British Aerospace plc. The autI!ors would especially like to acknowledge the in ut of Gerald Flanagan, Grumman Aircraft gystems Division, who made available his inhouse research on shear deformation theory applied to composite anels which was a valuable guide in &veloping the present anal sis. Also they wish to t ank Professor F. d Williams, University of Wales College df Cardiff for suggesting the problem and his consultation in the analysis development.

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