This paper documents the development of a conceptual level integrated process for design and analysis of efficient and environmentally acceptable supersonic aircraft. To overcome the technical challenges to achieve this goal, a conceptual design capability which provides users with the ability to examine the integrated solution between all disciplines and facilitates the application of multidiscipline design, analysis, and optimization on a scale greater than previously achieved, is needed. The described capability is both an interactive design environment as well as a high powered optimization system with a unique blend of low, mixed and high-fidelity engineering tools combined together in the software integration framework, ModelCenter. The various modules are described and capabilities of the system are demonstrated. The current limitations and proposed future enhancements are also discussed.


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    Titel :

    Integration of Multifidelity Multidisciplinary Computer Codes for Design and Analysis of Supersonic Aircraft


    Beteiligte:
    Geiselhart, Karl A. (Autor:in) / Ozoroski, Lori P. (Autor:in) / Fenbert, James W. (Autor:in) / Shields, Elwood W. (Autor:in) / Li, Wu (Autor:in)

    Kongress:

    49th AIAA Aerospace Sciences Meeting ; 2011 ; Orlando, FL, United States


    Erscheinungsdatum :

    2011-01-04


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    INTEGRATION OF MULTIFIDELITY MULTIDISCIPLINARY COMPUTER CODES FOR DESIGN AND ANALYSIS OF SUPERSONIC AIRCRAFT

    Geiselhart, K. / Ozoroski, L. / Fenbert, J. et al. | British Library Conference Proceedings | 2011





    Multifidelity Modeling Framework for Bayesian-Based Multidisciplinary Aircraft Design Optimization

    Kordonowy, David / Fitzgerald, Nathan / McClellan, Justin et al. | AIAA | 2012