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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    Title :

    The Lateral Stability of Aeroplanes


    Subtitle :

    Derivative Calculation by the Lotz System


    Contributors:
    Price, H.L. (author)

    Published in:

    Publication date :

    1943-12-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Lateral stability of aeroplanes

    Price, H.L. | Engineering Index Backfile | 1943


    Lateral stability in aeroplanes

    Levick, C. | Engineering Index Backfile | 1918


    The Lateral Stability of Aeroplanes

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


    The Lateral Stability of Aeroplanes

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


    The Lateral Stability of Aeroplanes

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