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A simple rectangular element for 2-dimensional analysis of laminated compositesA simple rectangular finite element was developed for two dimensional analysis of laminated composite materials. The rectangular laminated composite element eliminates the need to add elements to a model simply to account for the material properties of various laminae. This is particularly advantageous for thick laminates with many lamina. Explicit integration in terms of generalized displacements minimizes the algebraic effort required to derive the element stiffness and the thermal load vector. A substitute shape function technique is used to improve the performance of the element in modeling bending type deformation. Results for several example problems are discussed.
Document ID
19840024369
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Whitcomb, J. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-86291
NAS 1.15:86291
Report Number: NASA-TM-86291
Report Number: NAS 1.15:86291
Accession Number
84N32439
Funding Number(s)
PROJECT: RTOP 505-33-33-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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