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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 (AIAA 2015-1234)


    Contributors:

    Conference:

    Aerospace sciences meeting



    Publication date :

    2015-01-01


    Size :

    11 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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