Three-dimensional Navier-Stokes simulations are made for the external flow, the jet-exhaust plume, and the internal nozzle flow of a nonaxisymmetric nozzle typical of those advocated for advanced fighter airplanes. Solutions are presented for free-stream Mach numbers of 0.80, 0.94, and 1.20 at an angle of attack of 0 deg and a Reynolds number of 20 x 10 to the 6th. Jet-total-pressure ratios ranging from 1.5 to 9.8, i.e., from below to above the design pressure ratio of 4.25, are investigated. The results are compared to wind-tunnel data. The calculations successfully predict many trends and features of the external and internal flow.


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    Titel :

    Navier-Stokes simulation of nozzle-afterbody flows with jets at off-design conditions


    Beteiligte:

    Kongress:

    AIAA Applied Aerodynamics Conference


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Navier-Stokes Simulation of Nozzle-Afterbody Flows With Jets at Off-Design Conditions

    Compton, W. / Abdol-Hamid, K. / AIAA | British Library Conference Proceedings | 1991


    Navier-Stokes simulation of nozzle-afterbody flows with jets at off-design conditions

    COMPTON, III, WILLIAM / ABDOL-HAMID, KHALED | AIAA | 1991


    3-D Navier-Stokes Simulation of Turbulent Afterbody / Nozzle Flows

    Hamed, A. / Yeuan, J. J. / Liang, T. et al. | British Library Conference Proceedings | 1998


    3-D Navier-Stokes simulation of turbulent afterbody/nozzle flows

    Hamed, A. / Yeuan, J. / Liang, T. et al. | AIAA | 1998


    NAVIER-STOKES COMPUTATIONS ON NOZZLE-AFTERBODY CONFIGURATIONS

    Gogoi, A. / Rao, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003