Results of tests made in Langley free flight tunnel on free flying dynamic model.


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    Title :

    Experimental determination of effects of dihedral, vertical-tail area, and lift coefficient on lateral stability and control characteristics


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1946


    Size :

    24 pages


    Remarks:

    16 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :