The CAS22 computer program developed to provide for fast design and analysis of shock free airfoil cascades. CAS22 applicable to aerodynamic analysis and transonic shock free redesign of existing two-dimensional cascades of airfoils. Program is written in FORTRAN IV.


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    Title :

    Shock Free Airfoil Cascades


    Contributors:

    Published in:

    Publication date :

    1983-08-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



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