Simplified Methods for Determining Stresses and Deflections of Thin Laminated Composite Plates

770452

02/01/1977

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
This paper contains the results from three different methods for determining deflections and stress resultants of thin laminated composite plates subjected to lateral loads and uniform temperature changes. The first method is a classical method using the method of Ritz, and the results are considered exact; however, this method is cumbersome and not practical. The other two methods are more practical but in many instances produce approximate results. Each of these two simplified methods reduces the composite to a single orthotropic layer which is “equivalent” to the composite. The results from the two simplified methods are compared with the results from the exact method.
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DOI
https://doi.org/10.4271/770452
Pages
8
Citation
Smith, B., "Simplified Methods for Determining Stresses and Deflections of Thin Laminated Composite Plates," SAE Technical Paper 770452, 1977, https://doi.org/10.4271/770452.
Additional Details
Publisher
Published
Feb 1, 1977
Product Code
770452
Content Type
Technical Paper
Language
English