We begin by recalling the classical approach to solve shape design problems by gradient methods. Then we proceed to explain how automatic differentiation can simplify the analysis and illustrate this approach to a shape design problem where the shock is required to be at a certain place. The object of this chapter is to show that automatic differentiation seems to work even though the gradients and the calculus of variation have to be extended by Distribution theory.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Shock Optimization for Airfoil Design Problems


    Weitere Titelangaben:

    Springer Optimization


    Beteiligte:


    Erscheinungsdatum :

    2009-06-15


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Shock Optimization for Airfoil Design Problems

    Pironneau, O. | British Library Conference Proceedings | 2009


    Airfoil design by optimization

    RAMAMOORTHY, P. / PADMAVATHI, K. | AIAA | 1977


    Shock Free Airfoil Cascades

    Dulikravich, D. S. | NTRS | 1983



    Airfoil Optimization

    Per Krantz / Sven G. Hedman | AIAA | 1986