Simple method devised by which effect of wing elasticity on effective dihedral and on derivative in rolling moment coefficient due to sideslip may readily be determined for wings of various aspect ratios and taper ratios when different shapes of bending deflection curve are assumed.


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    Title :

    Effect of wing bending deflection on rolling moment due to sideslip


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :