The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
2015-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2015
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