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Lifetime Reliability Prediction of Ceramic Structures Under Transient Thermomechanical LoadsAn analytical methodology is developed to predict the probability of survival (reliability) of ceramic components subjected to harsh thermomechanical loads that can vary with time (transient reliability analysis). This capability enables more accurate prediction of ceramic component integrity against fracture in situations such as turbine startup and shutdown, operational vibrations, atmospheric reentry, or other rapid heating or cooling situations (thermal shock). The transient reliability analysis methodology developed herein incorporates the following features: fast-fracture transient analysis (reliability analysis without slow crack growth, SCG); transient analysis with SCG (reliability analysis with time-dependent damage due to SCG); a computationally efficient algorithm to compute the reliability for components subjected to repeated transient loading (block loading); cyclic fatigue modeling using a combined SCG and Walker fatigue law; proof testing for transient loads; and Weibull and fatigue parameters that are allowed to vary with temperature or time. Component-to-component variation in strength (stochastic strength response) is accounted for with the Weibull distribution, and either the principle of independent action or the Batdorf theory is used to predict the effect of multiaxial stresses on reliability. The reliability analysis can be performed either as a function of the component surface (for surface-distributed flaws) or component volume (for volume-distributed flaws). The transient reliability analysis capability has been added to the NASA CARES/ Life (Ceramic Analysis and Reliability Evaluation of Structures/Life) code. CARES/Life was also updated to interface with commercially available finite element analysis software, such as ANSYS, when used to model the effects of transient load histories. Examples are provided to demonstrate the features of the methodology as implemented in the CARES/Life program.
Document ID
20050237907
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Nemeth, Noel N.
(NASA Glenn Research Center Cleveland, OH, United States)
Jadaan, Osama J.
(Wisconsin Univ. Platteville, WI, United States)
Gyekenyesi, John P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
September 1, 2005
Subject Category
Structural Mechanics
Report/Patent Number
E-14061
NASA/TP-2005-212505
Report Number: E-14061
Report Number: NASA/TP-2005-212505
Funding Number(s)
WBS: WBS 22-708-31-09
Distribution Limits
Public
Copyright
Public Use Permitted.
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