Formula derived for pressure distribution under assumption of ratio of span to average chord (aspect ratio) that is not too small; range of validity of formula, so far as aspect ratio limitations are concerned, is not less than range of validity of lifting line theory for non-oscillating wing.


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    Titel :

    Effect of finite span on airload distributions for oscillating wings -- I: aerodynamic theory of oscillating wings of finite span


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Reissner, E. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :