Program aids in design of shockless airfoils, assists development of fuel-conserving, supercritical wings. Algorithm calculates approximate airfoil shape given prescribed pressure distribution. This allows design of families of transonic airfoils for use in aircraft wings or turbine and compressor blades. Program is written in FORTRAN IV for batch execution on CDC-6000.


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    Titel :

    Transonic airfoil design code


    Beteiligte:
    Bauer, F. (Autor:in) / Garabedian, P. (Autor:in) / Korn, D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1980-08-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Transonic Airfoil Analysis

    Holst, T. L. / Dougherty, F. C. / Gundy, K. L. et al. | NTRS | 1984