NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Multiple Concentric Cylinder Model (MCCM) user's guideA user's guide for the computer program mccm.f is presented. The program is based on a recently developed solution methodology for the inelastic response of an arbitrarily layered, concentric cylinder assemblage under thermomechanical loading which is used to model the axisymmetric behavior of unidirectional metal matrix composites in the presence of various microstructural details. These details include the layered morphology of certain types of ceramic fibers, as well as multiple fiber/matrix interfacial layers recently proposed as a means of reducing fabrication-induced, and in-service, residual stress. The computer code allows efficient characterization and evaluation of new fibers and/or new coating systems on existing fibers with a minimum of effort, taking into account inelastic and temperature-dependent properties and different morphologies of the fiber and the interfacial region. It also facilitates efficient design of engineered interfaces for unidirectional metal matrix composites.
Document ID
19940025620
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Williams, Todd O.
(Virginia Univ. Charlottesville, VA, United States)
Pindera, Marek-Jerzy
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1994
Subject Category
Composite Materials
Report/Patent Number
E-8689
NASA-CR-195299
NAS 1.26:195299
Report Number: E-8689
Report Number: NASA-CR-195299
Report Number: NAS 1.26:195299
Accession Number
94N30125
Funding Number(s)
CONTRACT_GRANT: NAS3-26571
PROJECT: RTOP 505-63-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available