Accession Number N20120012008
Title Development of Variable Camber Continuous Trailing Edge Flap System.
Publication Date Mar 2012
Media Count 16p
Personal Author J. Dykman J. Urnes N. T. Nguyen
Abstract 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.
Keywords Aeroelastic research wings
Cambered wings
Deflection
Drag reduction
Flight control
Flutter analysis
Shape memory alloys
Shape optimization
Trailing edge flaps


 
Source Agency National Aeronautics and Space Administration
NTIS Subject Category 51C - Aircraft
51F - Test Facilities & Equipment
Corporate Author National Aeronautics and Space Administration, Moffett Field, CA. Ames Research Center.
Document Type Technical report
Title Note N/A
NTIS Issue Number 1303
Contract Number NNL10AA16B

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