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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Airplane vibration -- Practical approach


    Additional title:

    SAE -- Business Aircraft Conf -- Proc


    Contributors:

    Conference:

    Proceedings of SAE -- Business Aircraft Conference ; 1965 Vibrations



    Publication date :

    1965


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Airplane Vibration - A Practical Approach

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


    Is the airplane diesel practical?

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


    Vibration response of airplane structures

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


    Part II. Practical Airplane Performance

    Lowry, John T. | AIAA | 1999


    Vibration response of airplane structures

    Theodorsen, T. / Gelalles, A. G. | TIBKAT | 1934