An Active Variable Camber Continuous Trailing Edge Flapped Wing Wind Tunnel Model for Aeroelastic ``In-Flight'' Shape Optimization Tests (AIAA 2018-3106)
19th AIAA/ISSMO multidisciplinary analysis and optimization conference 2018 ; 2018 ; Atlanta, GA
01.01.2018
18 pages
Aufsatz (Konferenz)
Englisch
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