The design of shockless airfoils that are appropriate for experimental work on a supersonic transport with an oblique wing are examined. A series of computer codes for the design and analysis of airfoils and wings in two dimensional and three dimensional transonic flow are studied. The oblique wing 3-D code was the forerunner of the later swept wing code. Techniques to incorporate the effect of an engine or fuselage in the inverse design code while using a minimum of computer resources are developed.


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    Titel :

    Study of transonic flow over swept wings


    Erscheinungsdatum :

    1983-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Transonic flow past swept wings

    Caughey, D. A. / Jameson, A. | NTRS | 1980


    Numerical calculation of transonic flow about swept wings

    BALLHAUS, W. / BAILEY, F. | AIAA | 1972


    Numerical Solution of Three-Dimensional Unsteady Transonic Flow over Swept Wings

    C. J. Borland / D. P. Rizzetta / H. Yoshihar | AIAA | 1982


    Transonic transport wings - Oblique or swept

    Jones, R. T. / Nisbet, J. W. | NTRS | 1974