Tests were conducted in the Ames 40 by 80 foot wind tunnel to determine the aerodynamic characteristics of a large-scale V/STOL aircraft model with thrust augmentors. The model had a double-delta wing of aspect ratio 1.65 with augmentors located in the wing root and the wing trailing edge. The supply air for the augmentor primary nozzles was provided by the YJ-97 turbojet engine. The airflow was apportioned approximately 74 percent to the wing root augmentor and 24 percent to wing augmentor. Results were obtained at several trailing-edge flap deflections with the nozzle jet-momentum coefficients ranging from 0 to 7.9. Three-component longitudinal data are presented with the agumentor operating with and without the horizontal tail. A limited amount of six component data are also presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wind-tunnel investigation of a large-scale VTOL aircraft model with wing root and wing thrust augmentors


    Beteiligte:
    Aoyagi, K. (Autor:in) / Aiken, T. N. (Autor:in)

    Erscheinungsdatum :

    1979-09-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Jet Wing with Multiple Thrust Augmentors

    H. J. P. Von Ohain / C. A. Scolatti | NTIS | 1971


    VTOL AIRCRAFT WING

    KIRIAKIDI SERGEJ KONSTANTINOVICH / POPOV DMITRIJ PAVLOVICH / TUPITSYN ALEKSANDR PAVLOVICH | Europäisches Patentamt | 2015

    Freier Zugriff

    CLOSED WING VTOL AIRCRAFT

    DE GRAAFF ARENT-JAN | Europäisches Patentamt | 2021

    Freier Zugriff

    Tilt-wing VTOL aircraft

    McCormick, Jr., B.W. / Mallen, J. | Engineering Index Backfile | 1957