Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    AIAA-2002-5597 Effects of Solver Fidelity on a Parallel Search Algorithm's Performance for Airfoil Shape Optimization Problems



    Kongress:

    Symposium; 9th, Multidisciplinary analysis and optimization ; 2002 ; Atlanta, GA



    Erscheinungsdatum :

    01.01.2002


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    AIAA-2019-3236: Multi-fidelity Efficient Global Optimization: Methodology And Application To Airfoil Shape Design

    Bartoli, Nathalie / Meliani, Mostafa / Morlier, Joseph et al. | British Library Conference Proceedings | 2019


    Adjoint-based Shape Optimization of High-lift Airfoil using the NSU2D Unstructured Mesh Solver (AIAA 2014-0554)

    Nambu, T. / Mavriplis, D.J. / Mani, K. et al. | British Library Conference Proceedings | 2014


    AIAA-2002-5602 Options for Robust Airfoil Optimization Under Uncertainty

    Padula, S. / Li, W. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2002