Three-dimensional thin-layer Navier-Stokes computations are presented for the F/A-18 configuration. The modeled configuration includes an accurate surface representation of the fuselage, leading-edge extension (LEX), and wing, both with and without leading-edge flap deflection. A multiblock structured grid strategy is employed to decompose the computational flowfield domain around the subject configuration. Steady-state solutions are obtained from an algorithm that solves the compressible Navier-Stokes equations with an upwind-biased, flux-difference splitting approach. The results presented are based on a fully turbulent flow assumption, simulating the high Reynolds number flow conditions that correspond to a recent FI A-18 flight experiment. Good agreements between the computations and the flight test results are obtained for both surface flow patterns as well as surface pressure distributions. Furthermore, a correlation between the computed LEX vortex-core and the flight test results, observed by way of smoke visualization, is also presented.


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    Titel :

    Multiblock Navier-Stokes Solutions About the F/A-18 Wing-Lex-Fuselage Configuration


    Beteiligte:
    Farhad Ghaffari (Autor:in) / James M Luckring (Autor:in) / James L Thomas (Autor:in) / Brent L Bates (Autor:in) / Robert T Biedron (Autor:in)

    Kongress:

    9th Applied Aerodynamics Conference ; 1991 ; Baltimore, MD, US


    Erschienen in:

    Erscheinungsdatum :

    1993-05-01




    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Multiblock Navier-Stokes solutions about the F/A-18 wing-LEX-fuselage configuration

    GHAFFARI, FARHAD / LUCKRING, JAMES M. / THOMAS, JAMES L. et al. | AIAA | 1993



    Multiblock Navier-Stokes solver for wing/fuselage transport aircraft

    Yang, G. / Kondo, M. / Obayashi, S. | Tema Archiv | 2002


    Navier-Stokes solutions about the F/A-18 wing-LEX-fuselage configuration with multi-block structured grids

    GHAFFARI, FARHAD / LUCKRING, JAMES / THOMAS, JAMES et al. | AIAA | 1991


    Navier-Stokes Solutions About the F/A-18 Wing-LEX-Fuselage Configuration with Multi-Block Structured Grids

    Ghaffari, F. / Luckring, J. / Thomas, J. et al. | British Library Conference Proceedings | 1991