In this paper, the bending singularity at the apex of a V-notched composite laminate plate is investigated. The anisotropy of the laminate is modeled by the Stroh formalism. Based on the eigenfunction expansion method, the bending singularity orders can be determined by solving an eigenvalue problem numerically. The singularity orders depend on the plate angle, material orientation, material anisotropy and the laminate stacking sequence. The comparison cases show that the material orientation should avoid in order to reduce the bending singularity. The layers near the free surfaces have more significant effects on the singularity order. The findings presented in this paper are helpful in the design of the composite laminate with V-notch.
|期刊||MATEC Web of Conferences|
|出版狀態||Published - 2018 二月 21|
|事件||2017 Asia Conference on Mechanical and Aerospace Engineering, ACMAE 2017 - Yokohama, Japan|
持續時間: 2017 十二月 29 → 2017 十二月 31
All Science Journal Classification (ASJC) codes
- Materials Science(all)