NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Effect of Stochastically Varying Creep Parameters on Residual Stresses in Ceramic Matrix CompositesConstituent properties, along with volume fraction, have a first order effect on the microscale fields within a composite material and influence the macroscopic response. Therefore, there is a need to assess the significance of stochastic variation in the constituent properties of composites at the higher scales. The effect of variability in the parameters controlling the time-dependent behavior, in a unidirectional SCS-6 SiC fiber-reinforced RBSN matrix composite lamina, on the residual stresses induced during processing is investigated numerically. The generalized method of cells micromechanics theory is utilized to model the ceramic matrix composite lamina using a repeating unit cell. The primary creep phases of the constituents are approximated using a Norton-Bailey, steady state, power law creep model. The effect of residual stresses on the proportional limit stress and strain to failure of the composite is demonstrated. Monte Carlo simulations were conducted using a normal distribution for the power law parameters and the resulting residual stress distributions were predicted.
Document ID
20160001351
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Pineda, Evan J.
(NASA Glenn Research Center Cleveland, OH United States)
Mital, Subodh K.
(Toledo Univ. Toledo, OH, United States)
Bednarcyk, Brett A.
(NASA Glenn Research Center Cleveland, OH United States)
Arnold, Steven M.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 2, 2016
Publication Date
January 5, 2015
Subject Category
Composite Materials
Structural Mechanics
Report/Patent Number
GRC-E-DAA-TN20022
AIAA Paper 2015-0389
Meeting Information
Meeting: AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SciTech 2015)
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Composites, American Society of Mechanical Engineers, American Society of Civil Engineers
Funding Number(s)
WBS: WBS 794072.02.03.03.03.02
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
processing
micromechanics
ceramic matrix composites
relaxation (mechanics)
residual stress
stastical analysis
residual stress
computational mechanics
thermal expansion
creep properties
No Preview Available