NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Optimization of Residual Stresses in MMC's through Process Parameter Control and the use of Heterogeneous Compensating/Compliant Interfacial Layers. OPTCOMP2 User's GuideA user's guide for the computer program OPTCOMP2 is presented in this report. This program provides a capability to optimize the fabrication or service-induced residual stresses in unidirectional metal matrix composites subjected to combined thermomechanical axisymmetric loading by altering the processing history, as well as through the microstructural design of interfacial fiber coatings. The user specifies the initial architecture of the composite and the load history, with the constituent materials being elastic, plastic, viscoplastic, or as defined by the 'user-defined' constitutive model, in addition to the objective function and constraints, through a user-friendly data input interface. The optimization procedure is based on an efficient solution methodology for the inelastic response of a fiber/interface layer(s)/matrix concentric cylinder model where the interface layers can be either homogeneous or heterogeneous. The response of heterogeneous layers is modeled using Aboudi's three-dimensional method of cells micromechanics model. The commercial optimization package DOT is used for the nonlinear optimization problem. The solution methodology for the arbitrarily layered cylinder is based on the local-global stiffness matrix formulation and Mendelson's iterative technique of successive elastic solutions developed for elastoplastic boundary-value problems. The optimization algorithm employed in DOT is based on the method of feasible directions.
Document ID
19970001593
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pindera, Marek-Jerzy
(Virginia Univ. Charlottesville, VA United States)
Salzar, Robert S.
(Virginia Univ. Charlottesville, VA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1996
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:198500
NASA-CR-198500
E-10314
Report Number: NAS 1.26:198500
Report Number: NASA-CR-198500
Report Number: E-10314
Accession Number
97N11387
Funding Number(s)
CONTRACT_GRANT: NAS3-26571
PROJECT: RTOP 505-65-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available