An investigation has been conducted in the Langley V/STOL tunnel to determine the low speed aerodynamic characteristics of a close-coupled canard-wing configuration using spanwise blowing and a vectored-engine-over-wing powered lift concept. The effects of spanwise blowing in conjunction with thrust vectoring are discussed. These effects were studied at M = 0.19 for a range of model angle of attack and engine nozzle pressure ratio. The results indicate combined use of spanwise blowing and thrust vectoring can provide significant performance improvements throughout the angle-of-attack range tested.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Low speed aerodynamic characteristics of a vectored-engine-over-wing configuration


    Beteiligte:
    Leavitt, L. D. (Autor:in) / Whitten, P. D. (Autor:in) / Stumpfl, S. C. (Autor:in)

    Kongress:

    Joint Propulsion Conference ; 1978 ; Las Vegas, NV, US


    Erscheinungsdatum :

    01.07.1978


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :