Method presented for determination of contour of disks, typified by those of aircraft gas turbines, to incorporate arbitrary elastic stress distributions resulting from either centrifugal or combined centrifugal and thermal effects. (15¢)


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    Title :

    Direct method of design and stress analysis of rotating disks with temperature gradient


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1950


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English