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Element Library for Three-Dimensional Stress Analysis by the Integrated Force MethodThe Integrated Force Method, a recently developed method for analyzing structures, is extended in this paper to three-dimensional structural analysis. First, a general formulation is developed to generate the stress interpolation matrix in terms of complete polynomials of the required order. The formulation is based on definitions of the stress tensor components in term of stress functions. The stress functions are written as complete polynomials and substituted into expressions for stress components. Then elimination of the dependent coefficients leaves the stress components expressed as complete polynomials whose coefficients are defined as generalized independent forces. Such derived components of the stress tensor identically satisfy homogenous Navier equations of equilibrium. The resulting element matrices are invariant with respect to coordinate transformation and are free of spurious zero-energy modes. The formulation provides a rational way to calculate the exact number of independent forces necessary to arrive at an approximation of the required order for complete polynomials. The influence of reducing the number of independent forces on the accuracy of the response is also analyzed. The stress fields derived are used to develop a comprehensive finite element library for three-dimensional structural analysis by the Integrated Force Method. Both tetrahedral- and hexahedral-shaped elements capable of modeling arbitrary geometric configurations are developed. A number of examples with known analytical solutions are solved by using the developments presented herein. The results are in good agreement with the analytical solutions. The responses obtained with the Integrated Force Method are also compared with those generated by the standard displacement method. In most cases, the performance of the Integrated Force Method is better overall.
Document ID
19960020433
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kaljevic, Igor
(Ohio Aerospace Inst. Cleveland, OH United States)
Patnaik, Surya N.
(Ohio Aerospace Inst. Cleveland, OH United States)
Hopkins, Dale A.
(NASA Lewis Research Center Cleveland,OH United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-4686
E-9522
NAS 1.15:4686
Report Number: NASA-TM-4686
Report Number: E-9522
Report Number: NAS 1.15:4686
Accession Number
96N24006
Funding Number(s)
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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