A graphical framework is used for statistical analysis of the results from an extensive N-version test of a collection of Reynolds-averaged Navier-Stokes computational fluid dynamics codes. The solutions were obtained by code developers and users from the U.S., Europe, Asia, and Russia using a variety of grid systems and turbulence models for the June 2009 4th Drag Prediction Workshop sponsored by the AIAA Applied Aerodynamics Technical Committee. The aerodynamic configuration for this workshop was a new subsonic transport model, the Common Research Model, designed using a modern approach for the wing and included a horizontal tail. The fourth workshop focused on the prediction of both absolute and incremental drag levels for wing-body and wing-body-horizontal tail configurations. This work continues the statistical analysis begun in the earlier workshops and compares the results from the grid convergence study of the most recent workshop with earlier workshops using the statistical framework.


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    Titel :

    Statistical Analysis of CFD Solutions from the Fourth AIAA Drag Prediction Workshop


    Beteiligte:
    J. H. Morrison (Autor:in)

    Erscheinungsdatum :

    2010


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Statistical Analysis of CFD Solutions from the Fourth AIAA Drag Prediction Workshop

    Morrison, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010


    Statistical Analysis of the Sixth AIAA Drag Prediction Workshop Solutions

    Derlaga, Joseph M. / Morrison, Joseph H. | AIAA | 2018