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    기술보고서 게시판 내용
    타이틀 Damage Tolerance and Reliability of Turbine Engine Components
    저자 Christos C. Chamis
    Keyword Probabilistic algorithms; Progressive fracture; Component reliability; Fault-tree
    URL http://gltrs.grc.nasa.gov/reports/1999/TP-1999-209878.pdf
    보고서번호 NASA TP-1999-209878
    발행년도 1999
    출처 NASA Glenn Research Center
    ABSTRACT This 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.

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