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The Boeing plastic analysis capability for enginesThe current BOPACE program is described as a nonlinear stress analysis program, which is based on a family of isoparametric finite elements. The theoretical, user, programmer, preprocessing aspects are discussed, and example problems are included. New features in the current program version include substructuring, an out-of-core Gauss wavefront equation solver, multipoint constraints, combined material and geometric nonlinearities, automatic calculation of inertia effects, provision for distributed as well as concentrated mechanical loads, follower forces, singular crack-tip elements, the SAIL automatic generation capability, and expanded user control over input quantity definition, output selection, and program execution. BOPACE is written in FORTRAN 4 and is currently available for both the IBM 360/370 and the UNIVAC 1108 machines.
Document ID
19770015584
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vos, R. G.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
December 25, 1976
Subject Category
Structural Mechanics
Report/Patent Number
D180-20229
NASA-CR-150246
Report Number: D180-20229
Report Number: NASA-CR-150246
Accession Number
77N22528
Funding Number(s)
CONTRACT_GRANT: NAS8-30615
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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