TY - JOUR
T1 - Complete solutions at or near the boundary nodes of boundary elements for coupled stretching-bending analysis
AU - Chang, H. W.
AU - Hwu, Chyanbin
N1 - Funding Information:
The authors would like to thank the Ministry of Science and Technology, Taiwan, Republic of China , for support through Grant MOST 104-2221-E-006-138-MY3 .
Publisher Copyright:
© 2016 Elsevier Ltd
PY - 2016/11/1
Y1 - 2016/11/1
N2 - In boundary element analysis if the field point is located at or near the boundary nodes, its associated integrals may become singular. Although in the literature the displacements and tractions at the boundary nodes have been well solved for the coupled stretching-bending analysis, their related strains and stresses still remain unsolved due to the coincidence of field points and boundary nodes. In this paper to avoid the singular problem, at the boundary nodes the components of stress resultants, bending moments, in-plane strains and plate curvatures in the tangential direction are approximated by finite difference method, whereas the components in normal direction are evaluated with the aid of constitutive laws for the tangential-normal coordinate. After getting the complete solutions at the boundary nodes, the solutions for the points near the boundary are interpolated by the moving least square method. To verify the correctness of the proposed method, examples of the laminated plates with or without holes subjected to in-plane tension, or out-of-plane bending, or transverse loading are illustrated and compared with the solutions obtained by the other methods.
AB - In boundary element analysis if the field point is located at or near the boundary nodes, its associated integrals may become singular. Although in the literature the displacements and tractions at the boundary nodes have been well solved for the coupled stretching-bending analysis, their related strains and stresses still remain unsolved due to the coincidence of field points and boundary nodes. In this paper to avoid the singular problem, at the boundary nodes the components of stress resultants, bending moments, in-plane strains and plate curvatures in the tangential direction are approximated by finite difference method, whereas the components in normal direction are evaluated with the aid of constitutive laws for the tangential-normal coordinate. After getting the complete solutions at the boundary nodes, the solutions for the points near the boundary are interpolated by the moving least square method. To verify the correctness of the proposed method, examples of the laminated plates with or without holes subjected to in-plane tension, or out-of-plane bending, or transverse loading are illustrated and compared with the solutions obtained by the other methods.
UR - https://www.scopus.com/pages/publications/84983782691
UR - https://www.scopus.com/pages/publications/84983782691#tab=citedBy
U2 - 10.1016/j.enganabound.2016.08.007
DO - 10.1016/j.enganabound.2016.08.007
M3 - Article
AN - SCOPUS:84983782691
SN - 0955-7997
VL - 72
SP - 89
EP - 99
JO - Engineering Analysis with Boundary Elements
JF - Engineering Analysis with Boundary Elements
ER -