Lift distribution produced by aileron deflections for rectangular wing on straight flight previously determined on theoretical principles for certain case, and air forces and moments produced by ailerons derived; approximate values deduced from former results for use in calculating acting forces and moments for all cases; results expressed by non-dimensional coefficients represented in diagrams. (See also Zeit. fuer Flugtechnik und Motorluftschiffahrt, vol. 19, no. 13, July 14, 1928, pp. 289-293, 10 figs)


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    Title :

    Determination of air forces and moments produced by ailerons of airplane


    Additional title:

    Bestimmung der durch die Querruder eines Tragfluegels erzeugten Luftkraefte und Momente


    Contributors:


    Publication date :

    1928


    Size :

    15 pages


    Remarks:

    10 Figs. on Supp. pp


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Determination of air forces and moments produced by ailerons of airplane

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    Forces and moments on airplane engine mounts

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