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SCBUCKLE user's manual: Buckling analysis program for simple supported and clamped panelsThe program SCBUCKLE calculates the buckling loads and mode shapes of cylindrically curved, rectangular panels. The panel is assumed to have no imperfections. SCBUCKLE is capable of analyzing specially orthotropic symmetric panels (i.e., A(sub 16) = A(sub 26) = 0.0, D(sub 16) = D(sub 26) = 0.0, B(sub ij) = 0.0). The analysis includes first-order transverse shear theory and is capable of modeling sandwich panels. The analysis supports two types of boundary conditions: either simply supported or clamped on all four edges. The panel can be subjected to linearly varying normal loads N(sub x) and N(sub y) in addition to a constant shear load N(sub xy). The applied loads can be divided into two parts: a preload component; and a variable (eigenvalue-dependent) component. The analysis is based on the modified Donnell's equations for shallow shells. The governing equations are solved by Galerkin's method.
Document ID
19930013515
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cruz, Juan R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:107741
NASA-TM-107741
Report Number: NAS 1.15:107741
Report Number: NASA-TM-107741
Accession Number
93N22704
Funding Number(s)
PROJECT: RTOP 505-63-50-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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