Basic wing had trapezoidal planform, aspect ratio of 3.0, taper ratio of 0.143, and unswept 80% chord line; modifications included deflectable full and partial span leading edge chord extensions; trapezoidal canard similar in planform to basic wing and 60° sweptback delta canard were tested; results obtained.


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    Title :

    Effects of canard planform and wing-leading-edge modification on low-speed longitudinal aerodynamic characteristics of canard airplane configuration


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    49 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :