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Why this result are not shell??? #65

@Myungjun-god

Description

@Myungjun-god

** 수정된 CalculiX용 입력 파일 (Abaqus 조건 반영)
*Heading
Unit system: MM_TON_S_C
**
** Nodes +++++++++++++++++++++++++++++++++++++++++
*Node
1, 10.0, 10.0, 0.0
2, 9.0, 10.0, 0.0
3, 8.0, 10.0, 0.0
4, 7.0, 10.0, 0.0
5, 6.0, 10.0, 0.0
6, 5.0, 10.0, 0.0
7, 4.0, 10.0, 0.0
8, 3.0, 10.0, 0.0
9, 2.0, 10.0, 0.0
10, 1.0, 10.0, 0.0
11, 0.0, 10.0, 0.0
12, 10.0, 9.0, 0.0
13, 9.0, 9.0, 0.0
14, 8.0, 9.0, 0.0
15, 7.0, 9.0, 0.0
16, 6.0, 9.0, 0.0
17, 5.0, 9.0, 0.0
18, 4.0, 9.0, 0.0
19, 3.0, 9.0, 0.0
20, 2.0, 9.0, 0.0
21, 1.0, 9.0, 0.0
22, 0.0, 9.0, 0.0
23, 10.0, 8.0, 0.0
24, 9.0, 8.0, 0.0
25, 8.0, 8.0, 0.0
26, 7.0, 8.0, 0.0
27, 6.0, 8.0, 0.0
28, 5.0, 8.0, 0.0
29, 4.0, 8.0, 0.0
30, 3.0, 8.0, 0.0
31, 2.0, 8.0, 0.0
32, 1.0, 8.0, 0.0
33, 0.0, 8.0, 0.0
34, 10.0, 7.0, 0.0
35, 9.0, 7.0, 0.0
36, 8.0, 7.0, 0.0
37, 7.0, 7.0, 0.0
38, 6.0, 7.0, 0.0
39, 5.0, 7.0, 0.0
40, 4.0, 7.0, 0.0
41, 3.0, 7.0, 0.0
42, 2.0, 7.0, 0.0
43, 1.0, 7.0, 0.0
44, 0.0, 7.0, 0.0
45, 10.0, 6.0, 0.0
46, 9.0, 6.0, 0.0
47, 8.0, 6.0, 0.0
48, 7.0, 6.0, 0.0
49, 6.0, 6.0, 0.0
50, 5.0, 6.0, 0.0
51, 4.0, 6.0, 0.0
52, 3.0, 6.0, 0.0
53, 2.0, 6.0, 0.0
54, 1.0, 6.0, 0.0
55, 0.0, 6.0, 0.0
56, 10.0, 5.0, 0.0
57, 9.0, 5.0, 0.0
58, 8.0, 5.0, 0.0
59, 7.0, 5.0, 0.0
60, 6.0, 5.0, 0.0
61, 5.0, 5.0, 0.0
62, 4.0, 5.0, 0.0
63, 3.0, 5.0, 0.0
64, 2.0, 5.0, 0.0
65, 1.0, 5.0, 0.0
66, 0.0, 5.0, 0.0
67, 10.0, 4.0, 0.0
68, 9.0, 4.0, 0.0
69, 8.0, 4.0, 0.0
70, 7.0, 4.0, 0.0
71, 6.0, 4.0, 0.0
72, 5.0, 4.0, 0.0
73, 4.0, 4.0, 0.0
74, 3.0, 4.0, 0.0
75, 2.0, 4.0, 0.0
76, 1.0, 4.0, 0.0
77, 0.0, 4.0, 0.0
78, 10.0, 3.0, 0.0
79, 9.0, 3.0, 0.0
80, 8.0, 3.0, 0.0
81, 7.0, 3.0, 0.0
82, 6.0, 3.0, 0.0
83, 5.0, 3.0, 0.0
84, 4.0, 3.0, 0.0
85, 3.0, 3.0, 0.0
86, 2.0, 3.0, 0.0
87, 1.0, 3.0, 0.0
88, 0.0, 3.0, 0.0
89, 10.0, 2.0, 0.0
90, 9.0, 2.0, 0.0
91, 8.0, 2.0, 0.0
92, 7.0, 2.0, 0.0
93, 6.0, 2.0, 0.0
94, 5.0, 2.0, 0.0
95, 4.0, 2.0, 0.0
96, 3.0, 2.0, 0.0
97, 2.0, 2.0, 0.0
98, 1.0, 2.0, 0.0
99, 0.0, 2.0, 0.0
100, 10.0, 1.0, 0.0
101, 9.0, 1.0, 0.0
102, 8.0, 1.0, 0.0
103, 7.0, 1.0, 0.0
104, 6.0, 1.0, 0.0
105, 5.0, 1.0, 0.0
106, 4.0, 1.0, 0.0
107, 3.0, 1.0, 0.0
108, 2.0, 1.0, 0.0
109, 1.0, 1.0, 0.0
110, 0.0, 1.0, 0.0
111, 10.0, 0.0, 0.0
112, 9.0, 0.0, 0.0
113, 8.0, 0.0, 0.0
114, 7.0, 0.0, 0.0
115, 6.0, 0.0, 0.0
116, 5.0, 0.0, 0.0
117, 4.0, 0.0, 0.0
118, 3.0, 0.0, 0.0
119, 2.0, 0.0, 0.0
120, 1.0, 0.0, 0.0
121, 0.0, 0.0, 0.0
**
** Elements ++++++++++++++++++++++++++++++++++++++
*Element, Type=S4, Elset=Set-1
1, 1, 2, 13, 12
2, 2, 3, 14, 13
3, 3, 4, 15, 14
4, 4, 5, 16, 15
5, 5, 6, 17, 16
6, 6, 7, 18, 17
7, 7, 8, 19, 18
8, 8, 9, 20, 19
9, 9, 10, 21, 20
10, 10, 11, 22, 21
11, 12, 13, 24, 23
12, 13, 14, 25, 24
13, 14, 15, 26, 25
14, 15, 16, 27, 26
15, 16, 17, 28, 27
16, 17, 18, 29, 28
17, 18, 19, 30, 29
18, 19, 20, 31, 30
19, 20, 21, 32, 31
20, 21, 22, 33, 32
21, 23, 24, 35, 34
22, 24, 25, 36, 35
23, 25, 26, 37, 36
24, 26, 27, 38, 37
25, 27, 28, 39, 38
26, 28, 29, 40, 39
27, 29, 30, 41, 40
28, 30, 31, 42, 41
29, 31, 32, 43, 42
30, 32, 33, 44, 43
31, 34, 35, 46, 45
32, 35, 36, 47, 46
33, 36, 37, 48, 47
34, 37, 38, 49, 48
35, 38, 39, 50, 49
36, 39, 40, 51, 50
37, 40, 41, 52, 51
38, 41, 42, 53, 52
39, 42, 43, 54, 53
40, 43, 44, 55, 54
41, 45, 46, 57, 56
42, 46, 47, 58, 57
43, 47, 48, 59, 58
44, 48, 49, 60, 59
45, 49, 50, 61, 60
46, 50, 51, 62, 61
47, 51, 52, 63, 62
48, 52, 53, 64, 63
49, 53, 54, 65, 64
50, 54, 55, 66, 65
51, 56, 57, 68, 67
52, 57, 58, 69, 68
53, 58, 59, 70, 69
54, 59, 60, 71, 70
55, 60, 61, 72, 71
56, 61, 62, 73, 72
57, 62, 63, 74, 73
58, 63, 64, 75, 74
59, 64, 65, 76, 75
60, 65, 66, 77, 76
61, 67, 68, 79, 78
62, 68, 69, 80, 79
63, 69, 70, 81, 80
64, 70, 71, 82, 81
65, 71, 72, 83, 82
66, 72, 73, 84, 83
67, 73, 74, 85, 84
68, 74, 75, 86, 85
69, 75, 76, 87, 86
70, 76, 77, 88, 87
71, 78, 79, 90, 89
72, 79, 80, 91, 90
73, 80, 81, 92, 91
74, 81, 82, 93, 92
75, 82, 83, 94, 93
76, 83, 84, 95, 94
77, 84, 85, 96, 95
78, 85, 86, 97, 96
79, 86, 87, 98, 97
80, 87, 88, 99, 98
81, 89, 90, 101, 100
82, 90, 91, 102, 101
83, 91, 92, 103, 102
84, 92, 93, 104, 103
85, 93, 94, 105, 104
86, 94, 95, 106, 105
87, 95, 96, 107, 106
88, 96, 97, 108, 107
89, 97, 98, 109, 108
90, 98, 99, 110, 109
91, 100, 101, 112, 111
92, 101, 102, 113, 112
93, 102, 103, 114, 113
94, 103, 104, 115, 114
95, 104, 105, 116, 115
96, 105, 106, 117, 116
97, 106, 107, 118, 117
98, 107, 108, 119, 118
99, 108, 109, 120, 119
100, 109, 110, 121, 120
**
** Node sets (Abaqus 파일의 노드 번호 기반 수정) +++++++++++++
** 1. 위쪽 면 (Loading): 1번부터 11번까지
*Nset, Nset=loading, generate
1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11
** 2. 왼쪽 면 (X-Symmetry): 11번부터 121번까지 11씩 증가 (X=0 라인)
*Nset, Nset=xsymm
11, 22, 33, 44, 55, 66, 77, 88, 99, 110, 121
** 3. 아래쪽 면 (Y-Symmetry): 111번부터 121번까지 (Y=0 라인)
*Nset, Nset=ysymm
111, 112, 113, 114, 115, 116, 117, 118, 119, 120, 121
** 4. 전체 노드 (안정성을 위한 Z축 구속용)
*Nset, Nset=allnodes, generate
1, 121, 1
**
** Materials & Sections (Abaqus 파일 두께 2.0 반영) ++++++++++
*Material, Name=Al
*Elastic
720000, 0.33
**
*Shell section, Elset=Set-1, Material=Al
1.0
**
** Step 시작 +++++++++++++++++++++++++++++++++++++++++++++++
*Step, nlgeom=YES
*Static
1.0, 1.0, 1E-05, 1.0
**
** Boundary conditions (Abaqus 로직 적용) +++++++++++++++++++
*Boundary
** Abaqus의 'xsymm, XSYMM'을 CalculiX용 DOF로 변환 (U1=0, UR2=0, UR3=0)
xsymm, 1, 1, 0
xsymm, 5, 6, 0
** Abaqus의 'ysymm, YSYMM'을 CalculiX용 DOF로 변환 (U2=0, UR1=0, UR3=0)
ysymm, 2, 2, 0
ysymm, 4, 4, 0
ysymm, 6, 6, 0
** Z축 방향 튀어나감 방지 (평면 유지)
allnodes, 3, 6, 0
** Abaqus의 'loading, 2, 2, 1.' 적용
loading, 2, 2, 1.0
**
** Output Requests +++++++++++++++++++++++++++++++++++++++++
*Node file
U, RF
*El file
S, E
**
*End step

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