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.
Development of Variable Camber Continuous Trailing Edge Flap System
NASA Fundamental Aeronautics 2012 Technical Conference ; 2012 ; Cleveland, OH, United States
13.03.2012
Sonstige
Keine Angabe
Englisch
British Library Conference Proceedings | 2015
|SAE Technical Papers | 2015
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