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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    Titel :

    Determination of air forces and moments produced by ailerons of airplane


    Weitere Titelangaben:

    Bestimmung der durch die Querruder eines Tragfluegels erzeugten Luftkraefte und Momente


    Beteiligte:
    Wieselsberger, C. (Autor:in) / Asano, T. (Autor:in)


    Erscheinungsdatum :

    1928


    Format / Umfang :

    15 pages


    Anmerkungen:

    10 Figs. on Supp. pp


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Determination of air forces and moments produced by ailerons of airplane

    Wieselsberger, C. / Asano, T. | Engineering Index Backfile | 1928


    Rolling, yawing, and hinge moments produced by rectangular ailerons

    Heald, R.H. | Engineering Index Backfile | 1933



    Forces and moments on airplane engine mounts

    Donely, P. | Engineering Index Backfile | 1936