Tests made in Langley free flight tunnel at lift coefficient of 1.0, covered range of geometric dihedral angles from -- 20 to 20° and range of vertical tail areas from 0 to 15% of wing area; results compared with previously reported results of similar series of tests on conventional model having wing with aspect ratio of 6.


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    Title :

    Lateral stability and control characteristics of free-flying model having unswept wing with aspect ratio of 2


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :