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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Parametric Powered-Lift Navier-Stokes Computations


    Beteiligte:
    N. M. Chaderjian (Autor:in) / S. Murman (Autor:in) / S. Pandya (Autor:in) / J. Ahmad (Autor:in)

    Erscheinungsdatum :

    2004


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Parametric Powered-Lift Navier-Stokes Computations

    Chaderjian, Neal M. / Murman, Scott / Pandya, Shishir et al. | NTRS | 2002




    Navier-Stokes computations of vortical flows

    DENG, G. / PIQUET, J. / QUEUTEY, P. | AIAA | 1990


    Wind Tunnel Experiments and Navier-Stokes Computations of a High-Lift Military Airfoil

    Dodbele, S. S. / Hobbs, C. R. / Kern, S. B. et al. | British Library Conference Proceedings | 1999