TY - JOUR
T1 - Theoretical equivalence and numerical performance of T3s and MITC3 plate finite elements
AU - Katili, Andi Makarim
AU - Maknun, Imam Jauhari
AU - Katili, Irwan
N1 - Publisher Copyright:
Copyright © 2019 Techno-Press, Ltd.
PY - 2019
Y1 - 2019
N2 - This paper will compare T3γs and MITC3 elements, both these two elements are three-node triangular plate bending elements with three degrees of freedom per node. The formulation of the T3γs and MITC3 elements is rather simple and has already been widely used. This paper will prove that the shear strain formulation of these two elements is identical even though they are obtained from two different methods. A single element is used to test the formulation of shear strain matrices. Numerical tests for circular plate cases compared with the exact solutions and with DKMT element will complete this review to verify the performances and show the convergence of these two elements.
AB - This paper will compare T3γs and MITC3 elements, both these two elements are three-node triangular plate bending elements with three degrees of freedom per node. The formulation of the T3γs and MITC3 elements is rather simple and has already been widely used. This paper will prove that the shear strain formulation of these two elements is identical even though they are obtained from two different methods. A single element is used to test the formulation of shear strain matrices. Numerical tests for circular plate cases compared with the exact solutions and with DKMT element will complete this review to verify the performances and show the convergence of these two elements.
KW - Assumed natural strain
KW - MITC3
KW - Plate bending element
KW - Reissner-Mindlin plate theory
KW - T3γs
UR - http://www.scopus.com/inward/record.url?scp=85062561926&partnerID=8YFLogxK
U2 - 10.12989/sem.2019.69.5.527
DO - 10.12989/sem.2019.69.5.527
M3 - Article
AN - SCOPUS:85062561926
SN - 1225-4568
VL - 69
SP - 527
EP - 536
JO - Structural Engineering and Mechanics
JF - Structural Engineering and Mechanics
IS - 5
ER -