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Completed Beltrami-Michell Formulation for Analyzing Radially Symmetrical BodiesA force method formulation, the completed Beltrami-Michell formulation (CBMF), has been developed for analyzing boundary value problems in elastic continua. The CBMF is obtained by augmenting the classical Beltrami-Michell formulation with novel boundary compatibility conditions. It can analyze general elastic continua with stress, displacement, or mixed boundary conditions. The CBMF alleviates the limitations of the classical formulation, which can solve stress boundary value problems only. In this report, the CBMF is specialized for plates and shells. All equations of the CBMF, including the boundary compatibility conditions, are derived from the variational formulation of the integrated force method (IFM). These equations are defined only in terms of stresses. Their solution for kinematically stable elastic continua provides stress fields without any reference to displacements. In addition, a stress function formulation for plates and shells is developed by augmenting the classical Airy's formulation with boundary compatibility conditions expressed in terms of the stress function. The versatility of the CBMF and the augmented stress function formulation is demonstrated through analytical solutions of several mixed boundary value problems. The example problems include a composite circular plate and a composite circular cylindrical shell under the simultaneous actions of mechanical and thermal loads.
Document ID
19950011784
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kaljevic, Igor
(Ohio Aerospace Inst. Cleveland, OH., United States)
Saigal, Sunil
(Carnegie-Mellon Univ. Pittsburgh, PA., United States)
Hopkins, Dale A.
(NASA Lewis Research Center Cleveland, OH, United States)
Patnaik, Surya N.
(Ohio Aerospace Inst. Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
E-8825
NAS 1.15:4593
NASA-TM-4593
Report Number: E-8825
Report Number: NAS 1.15:4593
Report Number: NASA-TM-4593
Accession Number
95N18199
Funding Number(s)
PROJECT: RTOP 505-63-53
Distribution Limits
Public
Copyright
Public Use Permitted.
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