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 Nat. Advisory Committee for Aeronautics -- Tech. Memo., no. 488, Nov. 1928, 15 pp., 10 figs. on supp. pp)


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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:

    Published in:

    Publication date :

    1928


    Size :

    5 pages


    Remarks:

    10 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


    Determination of air forces and moments produced by ailerons of airplane

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