SYMMETRIC AND ANTI-SYMMETRIC WING LOADING DISTRIBUTIONS IT is proposed to work out the span loading distribution and lift and drag coefficients of an unstalled wing in symmetric flight, together with the wing rolling and yawing derivatives for rolling and yawing flight. The only data assumed are a knowledge of the geometry of the wing and of the slope of the lift-incidence curve of any section of the wing when referred to infinite aspect ratio.


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    Titel :

    The Lateral Stability of Aeroplanes


    Untertitel :

    Derivative Calculation by the Lotz System


    Beteiligte:
    Price, H.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.12.1943


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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    The Lateral Stability of Aeroplanes

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    The Lateral Stability of Aeroplanes

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    The Lateral Stability of Aeroplanes

    Price, H.L. | Emerald Group Publishing | 1943