Exact mathematical treatment of problem is possible by replacing propeller blade by homogeneous prismatic rod; conclusions can then be drawn as to behavior of actual propeller; natural frequencies are determined and stressing of systems under various vibration modes are discussed. Indexed in Engineering Index 1939 p 50, from Deutsche Luftfahrtforschung Jahrbuch 1938 p II-141-59.


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    Title :

    Coupling of flexural propeller vibrations with torsional crankshaft vibrations


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Meyer, J. (author)


    Publication date :

    1943


    Size :

    46 pages


    Remarks:

    9 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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