The highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Section Components, are presented. The five technical tasks of the program are reviewed. Results of several tasks are presented.


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    Title :

    Pre-HOST high temperature crack propagation


    Contributors:


    Publication date :

    1982-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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