The goal of this work is to enable the computation of large numbers of unsteady high-fidelity flow simulations for a YAV-8B Harrier aircraft in ground effect by improving the solution process and taking advantage of NASA parallel supercomputers. The YAV-8B Harrier aircraft can take off and land vertically, or utilize short runways by directing its four exhaust nozzles toward the ground. Transition to forward flight is achieved by rotating these nozzles into a horizontal position.


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    Title :

    Parametric Powered-Lift Navier-Stokes Computations


    Contributors:
    N. M. Chaderjian (author) / S. Murman (author) / S. Pandya (author) / J. Ahmad (author)

    Publication date :

    2004


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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