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BUCLAP2: A computer program for instability analysis of laminated long plates subjected to combined inplane loadsThis program description document describes the program structure and the design details of a CDC 6600 FORTRAN 4 digital computer program, BUCLAP2, which uses minimum energy principles to do an elastic stability analysis of curved and flat laminated rectangular long plates subjected to combined inplane normal and shear loads. Given the geometry, the material properties, and slected boundary conditions for the plate element, the program calculates the minimum buckling load for various wave lengths. The two parallel ends of the program calculates the minimum buckling load for various wave lengths. The two parallel ends of the long plate must be simply supported and arbitrary elastic boundary conditions may be imposed along either one or both external longitudinal sides. For guide to program use, see
Document ID
19740005522
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Halstead, D. W. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Tripp, L. L. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Tamekuni, M. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Baker, L. L. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-132299
Accession Number
74N13635
Funding Number(s)
CONTRACT_GRANT: NAS1-11879
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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