Predicted on assumption of certain normal conditions, for engine and propeller, simple expressions for static and dynamic stresses of propeller blade roots are evolved. English translation of paper indexed in Engineering Index 1941 p 59, from Luftfahrtforschung Apr 22 1941.


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    Title :

    Design of propeller blade roots


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Cordes, G. (author)


    Publication date :

    1942


    Size :

    14 pages


    Remarks:

    4 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





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