The effect of deflected thrust on the stability and performance of a close-coupled canard fighter configuration are presented. These results were obtained at low speeds in the Langley V/STOL tunnel. Transonic as well as low-speed results are also presented for an unpowered close-coupled canard and a supercruiser configuration. The V/STOL tunnel data indicate an increase in maximum lift and reductions in drag due to lift with the addition of two-dimensional vectored thrust at the wing inboard trailing edge. The longitudinal pitchup associated with the unpowered configuration at higher angles of attack was significantly reduced with power.


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    Titel :

    Effects of deflected thrust on the stability and performance characteristics of a close-coupled canard fighter configuration


    Beteiligte:
    Thomas, J. L. (Autor:in) / Paulson, J. W., Jr. (Autor:in) / Yip, L. P. (Autor:in)

    Kongress:

    Propulsion Conference ; 1977 ; Orlando, FL, US


    Erscheinungsdatum :

    01.07.1977


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch