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Damage Tolerance and Reliability of Turbine Engine ComponentsThis report describes a formal method to quantify structural damage tolerance and reliability in the presence of a multitude of uncertainties in turbine engine components. The method is based at the material behavior level where primitive variables with their respective scatter ranges are used to describe behavior. Computational simulation is then used to propagate the uncertainties to the structural scale where damage tolerance and reliability are usually specified. Several sample cases are described to illustrate the effectiveness, versatility, and maturity of the method. Typical results from this method demonstrate that it is mature and that it can be used to probabilistically evaluate turbine engine structural components. It may be inferred from the results that the method is suitable for probabilistically predicting the remaining life in aging or deteriorating structures, for making strategic projections and plans, and for achieving better, cheaper, faster products that give competitive advantages in world markets.
Document ID
20000011913
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 1999
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TP-1999-209878
NAS 1.60:209878
E-11613
Report Number: NASA/TP-1999-209878
Report Number: NAS 1.60:209878
Report Number: E-11613
Meeting Information
Meeting: Qualification of Life Extension Schemes for Engine Components
Location: Corfu
Country: Greece
Start Date: October 5, 1998
End Date: October 9, 1998
Sponsors: North Atlantic Treaty Organization
Funding Number(s)
PROJECT: RTOP 523-22-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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