Theoretical mathematical study of influences of mass moment of inertia on blade when, in addition to rotation of blade around its axis fixed in aircraft, turning of whole aircraft around another spatially fixed axis takes place; calculation of torsonial oscillations.


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    Title :

    Inertia effects in propellers of aircraft in curving flight


    Additional title:

    Die Traegheitswirkungen in der Luftschraube des kurvenden Flugzeugs


    Contributors:
    Grammel, R. (author)

    Conference:

    Deutsche Akademie der Luftfahrtforschung -- Schriften Meeting ; 1941 Vibrations



    Publication date :

    1941


    Size :

    23 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    German




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    Free access