A state-of-the-art finite difference boundary-layer program incorporated into the NYU Transonic Analysis Program is described. Some possible treatments for the trailing edge region were investigated. Findings indicate the trailing edge region, still within the scope of an iterative potential flow, boundary layer program, appears feasible.


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    Title :

    Generalization of analytical tools for helicopter-rotor airfoils


    Contributors:

    Publication date :

    1979-04-18


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :