This presentation describes the advances being made with the Aerodynamic Shape Optimization (ASO) and high-fidelity Multidisciplinary Optimization (MDO) software used in the High Speed Research Program at NASA Ames Research Center. The description starts with the motivation for continued ASO/MDO development. Objectives of the current work are then presented. A list of ingredients deemed necessary for a flexible design environment is discussed, and the HSR requirement for different geometries at different design points is explained. Multiple design disciplines within a high-fidelity design environment are demonstrated. Finally, progress so far is summarized and planned future work is outlined.


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    Titel :

    Multi-Configuration and Aeroelastic Shape Design


    Beteiligte:
    Reuther, James (Autor:in) / Alonso, Juan J. (Autor:in) / Smith, Steve (Autor:in)


    Erscheinungsdatum :

    01.12.1999


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    CONTINUUM SENSITIVITY METHOD FOR AEROELASTIC SHAPE DESIGN PROBLEMS

    Liu, S. / Canfield, R. / American Institute of Aeronautics and Astronautics; International Society for Structural and Multidisciplinary Optimization | British Library Conference Proceedings | 2012


    Wing Design by Aerodynamic and Aeroelastic Shape Optimisation

    Morris, A. / Allen, C. / Rendall, T. et al. | British Library Conference Proceedings | 2008