Stability and Control Characteristics of Complete Airplane Model Having Wing with Quarter-Chord Line Swept Back 40°, Aspect Ratio 2.50, and Taper Ratio 0.42.


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    Title :

    Stability and control characteristics of complete airplane model having wing with quarter-chord line swept back 40°, aspect ratio 2.50, and taper ratio 0.42


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1951


    Size :

    86 pages


    Remarks:

    Illus, Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :