池鸿刚
Sophie,Rui Yang,张凯航
张凯航
2024-11-15
机械制造与自动化
J
53
05
102-107
1671-5276
multi-objective optimization; NSGA-Ⅱ; static strength test; wing wind-tunnel model
32-1643/TH
Pre One:MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON’S RATIO HONEYCOMB
Next One:Design and Experiment of a Water Hydraulic Artificial Muscle Actuated Diving Auxiliary Operating System