Issue 73
N. Laouche et alii, Fracture and Structural Integrity, 73 (2025) 88-107; DOI: 10.3221/IGF-ESIS.73.07
N 1 1 j
cos
x
(27)
j
The relation between and ത , and ഥ is defined using rule DQ [8]: b s z b s z u Qu w Qw , , , , ,
(28)
where
1
0
0
0
0
1
1 1,2
1 1,3
1
1
A A A
A A
N
N
1,1
1,
1
1, 0
0
0
1
0
Q
(29)
0
0
0
0
1
1
1
1
1
1
N N A A A ,1 ,2
N N A A , 1
N
N N ,
,3
Utilizing the DQFEM, by substituting Eqns. (21-29) into Eqns. (8, 12, 14) and employing Lagrange’s principle, we derive the subsequent elementaries matrixes. The element mass matrix:
e e e e e e e e e
M J Q CQ M J Q CA Q M J Q CA Q M JQCG JQA CA Q M M JQCG JQA CA Q M J Q CQ M JQG JQA CA Q 1 11 (1) 2 12 (1) 3 13 (1) (1) 1 5 22 (1) (1) 1 4 23 8 24 (1) (1) T T T T T T T T b T T s T T T
e
(30)
s
1
6
33
M J Q CQ M J Q CQ 8 34 T T
7
44
The element strain matrix:
95
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