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:
    J. Urnes (Autor:in) / N. T. Nguyen (Autor:in) / J. Dykman (Autor:in)

    Erscheinungsdatum :

    2012


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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