This is a report of work in support of the Computational Aerosciences (CAS) element of the Federal HPCC program. Specifically, CFD and aerodynamic optimization are being performed on parallel computers. The long-range goal of this work is to facilitate teraflops-rate multidisciplinary optimization of aerospace vehicles. This year's work is targeted for application to the High Speed Civil Transport (HSCT), one of four CAS grand challenges identified in the HPCC FY 1995 Blue Book. This vehicle is to be a passenger aircraft, with the promise of cutting overseas flight time by more than half. To meet fuel economy, operational costs, environmental impact, noise production, and range requirements, improved design tools are required, and these tools must eventually integrate optimization, external aerodynamics, propulsion, structures, heat transfer, controls, and perhaps other disciplines. The fundamental goal of this project is to contribute to improved design tools for U.S. industry, and thus to the nation's economic competitiveness.


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    Titel :

    High speed civil transport aerodynamic optimization


    Beteiligte:
    Ryan, James S. (Autor:in)

    Erscheinungsdatum :

    1994-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Variable-complexity aerodynamic optimization of a high-speed civil transport wing

    Hutchison, M. G. / Unger, E. R. / Mason, W. H. et al. | AIAA | 1994


    Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil Transport

    Susan E. Cliff / James J. Reuther / David A. Saunders et al. | AIAA | 2001


    Combined Aerodynamic and Structural Optimization of a high-Speed Civil Transport Wing

    Rohl, P. / Mavris, D. / Schrage, D. et al. | British Library Conference Proceedings | 1995