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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    Title :

    Development of Variable Camber Continuous Trailing Edge Flap System


    Contributors:

    Conference:

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


    Publication date :

    2012-03-13


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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