This presentation describes the current status of the joint NASA/Boeing collaboration on the development of a variable camber continuous trailing edge flap system for use in wing shaping control for cruise drag reduction.


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    Titel :

    Development of Variable Camber Continuous Trailing Edge Flap System


    Beteiligte:
    Urnes, Jim, Sr. (Autor:in) / Nguyen, Nhan T. (Autor:in) / Dykman, John (Autor:in)

    Kongress:

    NASA Fundamental Aeronautics 2012 Technical Conference ; 2012 ; Cleveland, OH, United States


    Erscheinungsdatum :

    13.03.2012


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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