The results of low cycle fatigue testing on turbine blades for use in hydrogen/oxygen rocket engines is presented. Cored blade and cored blades with circulation were tested in the MSFC thermal fatigue tester. Both blade configurations showed significant low cycle fatigue life improvements when compared to baseline solid blades.


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    Title :

    Turbine blade thermal fatigue testing Pratt and Whitney aircraft hollow core blades


    Contributors:
    Ingram, J. (author) / Gross, L. (author)

    Publication date :

    1985-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English