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Accession Number
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N20120012008
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Title
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Development of Variable Camber Continuous Trailing Edge Flap System.
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Publication Date
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Mar 2012
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Media Count
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16p
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Personal Author
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J. Dykman J. Urnes N. T. Nguyen
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Abstract
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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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Keywords
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Aeroelastic research wings
Cambered wings
Deflection
Drag reduction
Flight control
Flutter analysis
Shape memory alloys
Shape optimization
Trailing edge flaps
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Source Agency
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National Aeronautics and Space Administration
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NTIS Subject Category
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51C - Aircraft
51F - Test Facilities & Equipment
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Corporate Author
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National Aeronautics and Space Administration, Moffett Field, CA. Ames Research Center.
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Document Type
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Technical report
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Title Note
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N/A
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NTIS Issue Number
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1303
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Contract Number
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NNL10AA16B
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