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Dynamic response of laminated composite plates using a three-dimensional hybrid-stress finite-element formulationA method of analysis of dynamic response of laminated composite plates is presented. The analysis is carried by using a hybrid-stress finite element numerical technique. By using this approach, the response of simply supported laminated plates subjected to sinusoidal loading are investigated. For the solution of the finite element equations of motion of free vibrations and dynamic response problems, two effective methods of solution, the space iteration method and the Newmark direct integration method are used. These two methods are discussed here.
Document ID
19880004257
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liou, W. J.
(Feng Chia Univ. Taichung, Taiwan)
Sun, C. T.
(Florida Univ. Gainesville., United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA-Marshall Space Flight Center, The 58th Shock and Vibration Symposium, Volume 1
Subject Category
Composite Materials
Accession Number
88N13639
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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