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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    Titel :

    Generalization of analytical tools for helicopter-rotor airfoils


    Beteiligte:
    Gibbs, E. H. (Autor:in)

    Erscheinungsdatum :

    18.04.1979


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





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