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
2018-01-01
18 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2015
|