Program uses higher-order far field drag minimization. Computer program WDES WDEM preliminary aerodynamic design tool for one or two interacting, subsonic lifting surfaces. Subcritical wing design code employs higher-order far-field drag minimization technique. Linearized aerodynamic theory used. Program written in FORTRAN IV.


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    Titel :

    Interactive Graphics Analysis for Aircraft Design


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1983-10-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Effects of interactive graphics on the aircraft design process

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    Aircraft scheduling : an interactive graphics approach

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    Freier Zugriff

    Improving aircraft conceptual design - A PHIGS interactive graphics interface for ACSYNT

    WAMPLER, S. / MYKLEBUST, A. / JAYARAM, S. et al. | AIAA | 1988


    QUICK Interactive Graphics Analysis

    Townsend, J. C. | NTRS | 1984