A stress analysis procedure is presented for a redesign of the Space Shuttle Main Engine high pressure fuel turbopump turbine blades. The analysis consists of the one-dimensional scoping analysis to support the design layout and the follow on three-dimensional finite element analysis to confirm the blade design at operating loading conditions. Blade life is evaluated based on high-cycle fatigue and low-cycle fatigue.


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    Title :

    Stress analysis and life prediction of gas turbine blade


    Additional title:

    Spannungsanalyse und Lebensdauervorhersage von Gasturbinenschaufeln


    Contributors:
    Hsiung, H.C. (author) / Dunn, A.J. (author) / Woodling, D.R. (author) / Loh, D.L. (author)

    Published in:

    AIAA-Papers ; Jul ; 1-6


    Publication date :

    1988


    Size :

    6 Seiten, 12 Bilder, 2 Tabellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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