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    Titel :

    Cross-stream Contributions to Wing Wake Free Shear Layers Using Particle Image Velocimetry: Challenges and Results (AIAA 2017-1461)


    Beteiligte:

    Kongress:

    55th AIAA Aerospace Sciences Meeting 2017 ; 2017 ; Grapevine, Texas



    Erscheinungsdatum :

    01.01.2017


    Format / Umfang :

    20 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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