An effective computer modelling approach to the study of aeroelastic characteristics of an aircraft composite wing with high aspect ratioFusheng Wang, Zhufeng Yue, Shengjun Qiao et al.|Mathematical and Computer Modelling of Dynamical Systems|2014Cited by 7
Reliability analysis of laminated composite under compression and shear loadsFusheng Wang, Zhufeng Yue, Junran Zhang et al.|Journal of Central South University|2012Cited by 5