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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1961


    Format / Umfang :

    49 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :