The ability to accurately predict vehicle performance without resorting to full-scale tests will be critical to future powered-lift aircraft projects. This paper summarizes efforts to predict the flow field about a powered-lift aircraft, the YAV-8B Harrier, in low level jet-borne flight by solution of the Reynolds-averaged Navier-Stokes equations. Results are compared with infrared images of the NASA YAV-8B Harrier V/STOL Systems Research Aircraft (VSRA) under similar flight conditions.


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    Titel :

    Numerical simulation of a complete STOVL aircraft in ground effect


    Beteiligte:

    Kongress:

    AIAA Applied Aerodynamics Conference


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Numerical Simulation of a Complete STOVL Aircraft in Ground Effect

    Smith, M. H. / Chawla, K. / Van Dalsem, W. R. et al. | British Library Conference Proceedings | 1993


    Numerical simulation of a complete STOVL aircraft in ground effect

    SMITH, MERRITT / CHAWLA, KALPANA / VAN DALSEM, WILLIAM | AIAA | 1991


    Numerical simulation of a complete STOVL aircraft in ground effect

    Smith, Merritt / Chawla, Kalpana / Van Dalsem, William | AIAA | 1993


    Numerical Simulation of a Complete STOVL Aircraft in Ground Effect

    Smith, M. / Van Dalsem, W. / Chawla, K. et al. | British Library Conference Proceedings | 1991


    Numerical simulation of a complete STOVL aifcraft in ground effect

    Smith, Merritt H. / Chawla, Kalpana / Van Dalsem, William R. | NTRS | 1993