Aerodynamic effects induced from vectoring an exhaust jet are investigated using a well established thin-layer Reynolds averaged Navier-Stokes code. This multiple block code has been modified to allow for the specification of jet properties at a block face. The applicability of the resulting code for thrust vectoring applications is verified by comparing numerically and experimentally determined pressure coefficient distributions for a jet-wing afterbody configuration with a thrust-vectoring 2-D nozzle. Induced effects on the body and nearby wing from thrust vectoring are graphically illustrated.


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    Titel :

    Numerical Simulation of Propulsion-Induced Aerodynamic Characteristics on a Wing-Afterbody Configuration with Thrust Vectoring


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Lan, C. Edward (Autor:in) / Tseng, Jack B. (Autor:in) / Krist, Steven E. (Autor:in)

    Kongress:

    Aerospace Atlantic Conference & Exposition ; 1991



    Erscheinungsdatum :

    01.04.1991




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch







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