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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    Title :

    Transonic airfoil design code


    Contributors:
    Bauer, F. (author) / Garabedian, P. (author) / Korn, D. (author)

    Published in:

    Publication date :

    1980-08-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Transonic airfoil design

    CAHN, M. S. / GARCIA, J. R. | AIAA | 1971


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    HIROSE, NAOKI / TAKANASHI, SUSUMU / KAWAI, NOBUHIRO | AIAA | 1987


    Transonic airfoil analysis and design

    Carlson, L. A. | NTRS | 1980


    Transonic Airfoil Analysis

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