NASA NTRS · 20120012008
Development of Variable Camber Continuous Trailing Edge Flap System
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.
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Urnes, Jim, Sr., Nguyen, Nhan T., Dykman, John. 2012-03-13. Development of Variable Camber Continuous Trailing Edge Flap System. https://ntrs.nasa.gov/citations/20120012008
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