A new optimization based design method is discussed. This method is based on integrating existing disciplinary analysis and sensitivity analysis techniques by means of generalized sensitivity equations. A generic design system implementing this method is described. The system is being used to design the configuration and internal structure of a supersonic transport wing for optimum performance. This problem combines the disciplines of linear aerodynamics, structures, and performance. Initial results which include the disciplines of aerodynamics and structures in a conventional minimum weight design under static aeroelastic constraints are presented.


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    Titel :

    Application of multidisciplinary optimization methods to the design of a supersonic transport


    Beteiligte:
    Barthelemy, J.-F. M. (Autor:in) / Coen, P. G. (Autor:in) / Wrenn, G. A. (Autor:in) / Riley, M. F. (Autor:in) / Dovi, A. R. (Autor:in) / Hall, L. E. (Autor:in)


    Erscheinungsdatum :

    01.02.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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