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    Title :

    Helicopter Blade NACA 8H12 Performance Prediction with Laminar-Turbulent Transition Effects: Integral Boundary-Layer and CFD Results compared with Experimental Data


    Contributors:

    Conference:

    53rd AIAA Aerospace Sciences Meeting



    Publication date :

    2015-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English