Results of force tests at low Reynolds numbers; for low and moderate lift coefficients, changes in geometric dihedral from -10° to 10° resulted in change in effective dihedral that was about 75% as great as that obtained for unswept wing of aspect ratio 6.


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    Title :

    Effect of geometric dihedral on aerodynamic characteristics of 40° swept-back wing of aspect ratio 3


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Maggin, B. (author) / Shanks, R.E. (author)


    Publication date :

    1946


    Size :

    10 pages


    Remarks:

    15 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :