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NOLIN: A nonlinear laminate analysis programA nonlinear, plane-stress, laminate analysis program, NOLIN, was developed which accounts for laminae nonlinearity under inplane shear and transverse extensional stress. The program determines the nonlinear stress-strain behavior of symmetric laminates subjected to any combination of inplane shear and biaxial extensional loadings. The program has the ability to treat different stress-strain behavior in tension and compression, and predicts laminate failure using any or all of maximum stress, maximum strain, and quadratic interaction failure criteria. A brief description of the program is presented including discussion of the flow of information and details of the input required. Sample problems and a complete listing of the program is also provided.
Document ID
19750010547
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kibler, J. J.
(Materials Sciences Corp. Blue Bell, PA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-2410
Report Number: NASA-CR-2410
Accession Number
75N18619
Funding Number(s)
CONTRACT_GRANT: NAS1-12492
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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