With the Bernoulli-Euler beam used as a theoretical model, qualitative relationships have been developed to predict the angular vibration from a prescribed linear vibration response. Based on laboratory and flight test data the overall accuracy of predictions is within +or-20% of the angular vibration measurement. Such a prediction capability may be considered very significant in that the prediction schemes are intended only for qualitative purposes. In addition, due to the difficulties in obtaining accurate angular measurements, the present vibration data are limited to a gross confirmation of predictions.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Prediction of the angular vibration of aircraft structures


    Weitere Titelangaben:

    Vorhersage der Winkelschwingung von Flugzeugbauteilen


    Beteiligte:
    Lee, J. (Autor:in) / Whaley, P.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    9 Seiten, 11 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Angular vibration survey of various aircraft

    Merritt, Paul / Donaldson, Jed / O'Brien, David et al. | SPIE | 2003


    Vibration Analysis of Aircraft Structures

    Hedgepeth, J. M. | NTRS | 1961


    MEASUREMENT and PREDICTION of AIRCRAFT VIBRATION

    CRITCHLOW, E. FOREST | SAE Technical Papers | 1944


    SEMI-ACTIVE VIBRATION CONTROL OF AIRCRAFT STRUCTURES

    Chatziathanasiou, Grigoris / Chrysohoidis, Nikolaos / Kostas, Georgopoulos et al. | TIBKAT | 2021


    Semi-Active Vibration Control of Aircraft Structures

    Chatziathanasiou, Grigoris / Chrysohoidis, Nikolaos / Kostas, Georgopoulos et al. | AIAA | 2021