Design, Construction, and Tests of an Aeroelastic Wind Tunnel Model of a Variable Camber Continuous Trailing Edge Flap (VCCTEF) Concept Wing (AIAA 2014-2442)
Conference; 32nd, Applied aerodynamics ; 2014 ; Atlanta, GA
01.01.2014
31 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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