Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design

This paper presents experimental results of a flexible wing wind tunnel model with a variable camber continuous trailing edge flap (VCCTEF) design for drag minimization, tested at the University of Washington Aeronautical Labo- ratory (UWAL). The wind tunnel test was designed to explore the relative...

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Bibliographische Detailangaben

Hauptverfasser:	Nguyen, Nhan T., Precup, Nathan, Urnes, James, Nelson, Chester, Lebofsky, Sonia, Ting, Eric Bi-Wen, Livne, Eli
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Design, Testing And Performance
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