In study of landing and takeoff problems of current designs and need for improved highlift devices, investigation was made at R 0.9×106 to determine longitudinal aerodynamic characteristics of flap; maximum lift coefficient of 2.2 was obtained with double slotted flap in conjunction with leading edge slat.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Investigation of double slotted flaps on swept-wing transport model


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Naeseth, R.L. (Autor:in) / Davenport, E.E. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Investigation of double slotted flaps on a swept-wing transport model

    Naeseth, Rodger L. / Davenport, Edwin E. | TIBKAT | 1959


    SLOTTED WING FLAPS FOR A VTOL AIRCRAFT

    KAREM ABE / PARCELL JOHN PAUL | Europäisches Patentamt | 2020

    Freier Zugriff

    Slotted Wing Flaps For A VTOL Aircraft

    KAREM ABE / PARCELL JOHN PAUL | Europäisches Patentamt | 2020

    Freier Zugriff


    Aircraft high lift device with double slotted flaps and fixed-wing aircraft

    ZOU XIANGFU / WANG JIANG / GUO JINGLIANG et al. | Europäisches Patentamt | 2023

    Freier Zugriff