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Development of Variable Camber Continuous Trailing Edge Flap SystemThis 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.
Document ID
20120012008
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Urnes, Jim, Sr. (Boeing Co. CA, United States)
Nguyen, Nhan T. (NASA Ames Research Center Moffett Field, CA, United States)
Dykman, John (Boeing Co. CA, United States)
Date Acquired
August 26, 2013
Publication Date
March 13, 2012
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN4940
Meeting Information
Meeting: NASA Fundamental Aeronautics 2012 Technical Conference
Location: Cleveland, OH
Country: United States
Start Date: March 13, 2012
Sponsors: NASA Headquarters
Funding Number(s)
CONTRACT_GRANT: NNL10AA16B
WBS: WBS 561581.02.08.01.46.02
Distribution Limits
Public
Copyright
Public Use Permitted.

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