Method described can be used to investigate possibility of flutter on such structures as airplane wings, tail surfaces, bomb doors, aircraft propeller blades, vehicular bridges, buildings, etc; with well known solution for air forces for two-dimensional flow over airfoil with aileron, equations were derived which can be used to determine flutter speed for wing or tail surfaces of any conventional airplane; use of still air vibration tests in obtaining structural friction of structures, and in checking part of flutter computations experimentally is indicated. (See also - discussion p 355-6)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    General approach to flutter problem


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Loring, S.J. (Autor:in)


    Erscheinungsdatum :

    1941


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    General Approach to the FLUTTER PROBLEM

    LORING, S. J. | SAE Technical Papers | 1941


    Simple approach to wing flutter problem

    Lockspeiser, B. | Engineering Index Backfile | 1933


    Mechanism of flutter -- Theoretical and experimental investigation of flutter problem

    Theodorsen, T. / Garrick, I.E. | Engineering Index Backfile | 1940


    An approach to the flutter problem in real fluids

    Rott, N. / George, M. B. T. | TIBKAT | 1955


    A General Method for Flutter Optimization

    L.B. GWIN AND R.F. TAYLOR | AIAA | 1973