Program analyzes airfoils that permit transonic flow for subsonic free-stream mach numbers. Transonic refers to aircraft speeds less than speed of sound, but close enough so that top of wing, where airflow is fastest, mach number becomes greater than 1. Program should aid design phase of new airfoil and in analysis of existing airfoils.


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    Title :

    Transonic flow about airfoils


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

    Published in:

    Publication date :

    1978-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Calculating Transonic Flows About Airfoils

    Seidel, David A. / Batina, John T. / Whitlow, Woodrow, Jr. | NTRS | 1989





    Inviscid transonic flow over airfoils

    MAGNUS, R. / YOSHIHARA, H. | AIAA | 1970