Investigations on a STOL-airplane with internally blown flaps are described. To avoid flow separation on the wing, slots were located behind the nose flap and in front of the trailing edge flap. Maximum lift and optimum L/D were investigated, as well as the effectiveness of the aileron and the horizontal tail. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Three Component Measurements on a Light STOL Aircraft with Chordwise Blowing


    Beteiligte:
    H. Koerner (Autor:in) / R. Loehr (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch








    STOL AIRCRAFT

    MOMBRINIE BRUNO | Europäisches Patentamt | 2020

    Freier Zugriff