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Nonlinear transient analysis by energy minimization: A theoretical basis for the ACTION computer codeThe formulation basis for establishing the static or dynamic equilibrium configurations of finite element models of structures which may behave in the nonlinear range are provided. With both geometric and time independent material nonlinearities included, the development is restricted to simple one and two dimensional finite elements which are regarded as being the basic elements for modeling full aircraft-like structures under crash conditions. Representations of a rigid link and an impenetrable contact plane are added to the deformation model so that any number of nodes of the finite element model may be connected by a rigid link or may contact the plane. Equilibrium configurations are derived as the stationary conditions of a potential function of the generalized nodal variables of the model. Minimization of the nonlinear potential function is achieved by using the best current variable metric update formula for use in unconstrained minimization. Powell's conjugate gradient algorithm, which offers very low storage requirements at some slight increase in the total number of calculations, is the other alternative algorithm to be used for extremely large scale problems.
Document ID
19800018198
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kamat, M. P.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-3287
Report Number: NASA-CR-3287
Accession Number
80N26697
Funding Number(s)
CONTRACT_GRANT: NSG-1546
CONTRACT_GRANT: NAS1-15080
CONTRACT_GRANT: NGR-47-004-114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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