Flexible airplane structures in presence of excitation forces may oscillate with bounded or unbounded motion; vehicle safety and durability depend on control and reduction of vibration; designers can generally safeguard against its occurrence by tuning airframe; supplementing design function are experimental studies that identify dynamic response characteristics for aeroelastic and fatigue considerations; experimental methodology, based on fundamental engineering principles and basic laboratory instrumentation, is described together with examples which demonstrate directness and efficiency obtainable.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Airplane vibration -- Practical approach


    Weitere Titelangaben:

    SAE -- Business Aircraft Conf -- Proc


    Beteiligte:
    Schultz, W.H. (Autor:in)

    Kongress:

    Proceedings of SAE -- Business Aircraft Conference ; 1965 Vibrations



    Erscheinungsdatum :

    1965


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Airplane Vibration - A Practical Approach

    Schultz, W. H. | SAE Technical Papers | 1965


    Practical airplane performance calculations

    Watter, M. | Engineering Index Backfile | 1930


    Is the airplane diesel practical?

    Cleveland, R.M. | Engineering Index Backfile | 1929


    Part II. Practical Airplane Performance

    Lowry, John T. | AIAA | 1999


    Vibration response of airplane structures

    Theodorsen, T. / Gelalles, A.G. | Engineering Index Backfile | 1934