This report presents a survey of previous theoretical and experimental investigations on wing flutter covering thirteen cases of flutter observed on airplanes. The direct cause of flutter is, in the majority of cases, attributable to (mass-) unbalanced ailerons. Under the conservative assumption that the flutter with the phase angle most favorable for excitation occurs only in two degrees of freedom, the lowest critical speed can be estimated from the data obtained on the oscillation bench. Corrective measures for increasing the critical speed and for definite avoidance of wing flutter, are discussed.


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    Titel :

    Status of wing flutter


    Beteiligte:
    Kussner, H G (Autor:in)

    Erscheinungsdatum :

    01.01.1936


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Status of wing flutter

    Küssner, H. G. | TIBKAT | 1936



    Supercritical Wing Flutter

    J. A. McGrew / J. P. Giesing / R. M. Pearson et al. | NTIS | 1978



    Aeroplane Wing Flutter

    Frazer, R.A. | Emerald Group Publishing | 1929