This paper demonstrates a simulation-based aerodynamic design process of high speed inlet. A genetic algorithm is integrated into the design process to facilitate the single objective optimization. The objective function is the total pressure recovery and is obtained by using a PNS solver for its computing efficiency. The system developed uses existing software of geometry definition, mesh generation and CFD analysis. The process which produces increasingly desirable design in each genetic evolution over many generations is automatically carried out. A generic two-dimensional inlet is created as a showcase to demonstrate the capabilities of this tool. A parameterized study of geometric shape and size of the showcase is also presented.


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    Titel :

    An Interactive Preliminary Design System of High Speed Forebody and Inlet Flows


    Beteiligte:

    Kongress:

    48th AIAA Aerospace Sciences Meeting ; 2010 ; Orlando, FL, United States


    Erscheinungsdatum :

    2010-01-04


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An Interactive Preliminary Design System of High Speed Forebody and Inlet Flows

    Liou, May-Fun / Benson, Thomas / Trefny, Charles | AIAA | 2010


    AN INTERACTIVE PRELIMINARY DESIGN SYSTEM OF HIGH SPEED FOREBODY AND INLET FLOWS

    Liou, M. / Benson, T. / Trefny, C. et al. | British Library Conference Proceedings | 2010


    Interactive Parabolized Navier-Stokes Solver for High Speed Forebody and Inlet Flows

    Benson, T. / Liou, M. / Jones, W. et al. | British Library Conference Proceedings | 2009


    Interactive Parabolized Navier-Stokes Solver for High Speed Forebody and Inlet Flows

    Benson, Thomas / Liou, May-Fun / Jones, William et al. | AIAA | 2009


    A New Combined Design of Inlet and forebody for High-speed Vehicle

    Huang, Guoping / Zhou, Miao / Chen, Jie et al. | AIAA | 2011