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Nonlinear mesomechanics of composites with periodic microstructureThis work is concerned with modeling the mechanical deformation or constitutive behavior of composites comprised of a periodic microstructure under small displacement conditions at elevated temperature. A mesomechanics approach is adopted which relates the microimechanical behavior of the heterogeneous composite with its in-service macroscopic behavior. Two different methods, one based on a Fourier series approach and the other on a Green's function approach, are used in modeling the micromechanical behavior of the composite material. Although the constitutive formulations are based on a micromechanical approach, it should be stressed that the resulting equations are volume averaged to produce overall effective constitutive relations which relate the bulk, volume averaged, stress increment to the bulk, volume averaged, strain increment. As such, they are macromodels which can be used directly in nonlinear finite element programs such as MARC, ANSYS and ABAQUS or in boundary element programs such as BEST3D. In developing the volume averaged or efective macromodels from the micromechanical models, both approaches will require the evaluation of volume integrals containing the spatially varying strain distributions throughout the composite material. By assuming that the strain distributions are spatially constant within each constituent phase-or within a given subvolume within each constituent phase-of the composite material, the volume integrals can be obtained in closed form. This simplified micromodel can then be volume averaged to obtain an effective macromodel suitable for use in the MARC, ANSYS and ABAQUS nonlinear finite element programs via user constitutive subroutines such as HYPELA and CMUSER. This effective macromodel can be used in a nonlinear finite element structural analysis to obtain the strain-temperature history at those points in the structure where thermomechanical cracking and damage are expected to occur, the so called damage critical points of the structure.
Document ID
19890016889
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Walker, Kevin P.
(Engineering Science Software, Inc., Smithfield RI., United States)
Jordan, Eric H.
(Connecticut Univ. Storrs., United States)
Freed, Alan D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1989
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:102051
NASA-TM-102051
E-4670
Report Number: NAS 1.15:102051
Report Number: NASA-TM-102051
Report Number: E-4670
Accession Number
89N26260
Funding Number(s)
CONTRACT_GRANT: NAG3-882
PROJECT: RTOP 553-13-00
PROJECT: RTOP 510-01-0A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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