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Shear buckling of specially orthotropic plates with centrally located cutoutsThere is significant industry demand for a method of analyzing the shear buckling of composite plates with cutouts. This method should be able to easily accommodate frequent changes in model design; inflexibility is the major drawback to current finite element methods. The approach taken here is broken into two problems, prebuckling and buckling. To solve for the prebuckling stresses, complex variable equations are used in conjunction with boundary collocation. The least squares approach is utilized to improve the accuracy of the results. The buckling problem is solved using the Ritz method. A product of the Ritz method is a complicated integral equation which is solved using numerical integration. To date, the aforementioned method of determining the prebuckling stresses was verified against infinite plate theory and finite elements.
Document ID
19920023345
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Owen, Vicki L.
(North Carolina State Univ. Raleigh, NC, United States)
Klang, Eric C.
(North Carolina State Univ. Raleigh, NC, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Publication Information
Publication: NASA. Langley Research Center, Eighth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Part 2
Subject Category
Composite Materials
Accession Number
92N32589
Funding Number(s)
CONTRACT_GRANT: NAG1-917
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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