PANAIR uses high-order panel method to predict inviscid subsonic or supersonic flows about arbitrary configuration. Panel method solves linear partial differential equation numerically by approximating configuration surface with panels on which unknown "singularity strengths" are defined. PANAIR includes advanced software technology as well as advanced aerodynamic technology.


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    Titel :

    Higher-Order Panel Method for Aerodynamic Flow Analysis


    Beteiligte:
    Erickson, L. (Autor:in) / Carmichael, R. L. (Autor:in) / Levin, A. D. (Autor:in) / Magnus, A. (Autor:in) / Epton, M. (Autor:in) / Baruah, P. (Autor:in) / Massena, B. (Autor:in) / Bussoletti, J. (Autor:in) / Sidwell, K. (Autor:in) / Johnson, F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1982-12-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic Evaluation of Wing-Strake Modification by Higher Order Panel Method

    Maqsood, Adnan / Masud, Jehanzeb / Mehdi, Abid | AIAA | 2007


    Aerodynamic Evaluation of Wing-Strake Modification by Higher Order Panel Method AIAA Paper

    Maqsood, A. / Masud, J. / Mehdi, A. et al. | British Library Conference Proceedings | 2007


    Aerodynamic Computations Using a Higher-Order Algorithm

    De Rango, S. / Zingg, D. W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1999


    Aerodynamic computations using a higher-order algorithm

    De Rango, S. / Zingg, D. | AIAA | 1999


    Improved Higher-Order Panel Method for Linearized Supersonic Flow

    F. E. Ehlers / M. A. Epton / F. T. Johnson et al. | AIAA | 1979