PROGRESS ON GUST LOAD ALLEVIATION WIND TUNNEL EXPERIMENT AND AEROSERVOELASTIC MODEL VALIDATION FOR A FLEXIBLE WING WITH VARIABLE CAMBER CONTINUOUS TRAILING EDGE FLAP SYSTEM
AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.
Structural dynamics ; Volume 1 of 2 ; 72-113
2020
Conference paper
English
British Library Conference Proceedings | 2015
|