引用次数
引用: 680
H-指数: 16
I10-指数 : 22
出版物: 51
Study on test method for aircraft rudder residual strength
Yuan Liang , Xiuhua Chen , Yin Yu , Hai Wang
Shiyan Jishu yu Guanli 28 ( 5) 44 -47
2011
EXPERIMENTAL AND NUMRICAL INVESTIGATION OF COMPOSITIES WITH SINGLE COUNTERSUNK JOINTS
Siyuan Yao , Xiuhua Chen , Xiaojing Zhang , Zhefeng Yu
PROGRESSIVE FAILURE ANALYSIS OF THE OPEN-HOLE COMPOSITES LAMINATES USING SFEM METHOD AND TEST VALIDATION
Xiuhua Chen , Yin Yu , Hai Wang1and Jian Zhao
REALIZING DOMAIN SUPERPOSITION TECHNIQUE IN NASTRAN FOR PREDICTING THE MECHANICAL PROPERTIES OF TEXTILE COMPOSITE
Xiuhua Chen , Yan Deng , Ming Li , Hai Wang
An optimization method for composite structures with ply-drops
Hai-Tao Fan , Hai Wang , Xiu-Hua Chen ,
Composite Structures 136 650 -661
41
2016
Fracture phase field modeling of 3D stitched composite with optimized suture design
Pu-Song Ma , Jia-Yu Ye , Kun Tian , Xiu-Hua Chen
Computer Methods in Applied Mechanics and Engineering 392 114650 -114650
18
2022
Modified Fick’s law and Tsai method applied to the analysis of adhesive bonded repaired composite
Yin Yu , Xiu-Hua Chen , Kun-Hua Han , Hai Wang
20th International Conference on Composite Materials Copenhagen
1
2015
The Residual Strength Test and Analysis of Composite Rudder After Lightning Strike
X Chen , G Liu , H Wang
the Proceedings of the 18th International Conference on Composite Materials
3
2011
Optimization Design and Nonlinear Bending of Bio-Inspired Helicoidal Composite Laminated Plates. Materials 2023, 16, 4550
T Lu , HS Shen , H Wang , X Chen
2023
Progressive Failure Analysis of an Open-Hole Composite Laminate by Using the S-Version Finite-Element Method
X. Chen , Z. Li , H. Wang
Mechanics of Composite Materials 50 ( 3) 279 -294
7
2014
Strength investigation of composite honeycomb structures after repair
Hai Wang , Xiu-hua Chen , Xing-lin Guo , Ming-fa Ren
Acta Aeronautica et Astronautica Sinica 22 ( 3) 270 -273
14
2001