This paper presents data from tests in a two-dimensional pressurized wind tunnel of two new wing sections suitable for light transport aircraft, and a NACA 633-418 airfoil. The two new airfoils had maximum thickness/chord ratios of 18% and 21% and they were designed to achieve improved high lift and low drag by exploiting considerable aft loading and blunt trailing edges.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Airfoils for Light Transport Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Teeling, P. (Autor:in) / Poole, R.J.D. (Autor:in)

    Kongress:

    Business Aircraft Meeting and Exposition ; 1981



    Erscheinungsdatum :

    1981-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch