有限元作业西北农林科技大学.docx
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有限元作业西北农林科技大学
目录
一.平面结构(木板应力分析)1
(一)木板计算图示1
(二)计算代码1
(三)运算结果2
二.桁架结构4
(一)桁架计算图示4
(二)计算代码4
(三)运算结果5
三.刚架结构6
(一)刚架计算图示6
(二)计算代码6
(三)运算结果7
四.钢筋混凝土框架结构简单分析9
(一)问题描述9
(二)前处理9
1.运行ANSYS9
2.定义单元类型9
3.定义材料属性9
4.几何模型9
5.划分网格10
(三)求解10
1.定义分析类型10
2.施加约束10
3.施加重力10
4.开始求解10
(四)后处理11
1.结构变形图11
2.位移云图11
3.主应力云图11
一.平面结构(木板应力分析)
木板尺寸为300mmX300mmX5mm,四角采用固定铰支座。
在结点8,9施加500N的竖向作用力,节点5,11施加500N的水平作用力,然后分析木板应力的变化。
先将木板平面分成36个单元,分别编上号码。
在记事本文件以一定的格式写入代码后,运用MATLAB软件进行应力分析。
(一)木板计算图示
(二)计算代码
PLATE
YangBoxing
NNNENMNDIMNENNDN
25361232
NDNLNMPC
840
NODE#XY
100
21000
32000
43000
5300100
6300200
7300300
8200300
9100300
100300
110200
120100
135050
1415050
1525050
16250150
17250250
18150250
1950250
2050150
21100100
22200100
23200200
24100200
25150150
Elem#Node1Node2Node3Material#ThicknessTempChange
11213150
211312150
3132112150
422113150
521421150
62314150
732214150
8142221150
931522150
103415150
114515150
1215522150
1322516150
141656150
1516623150
16221623150
17212225150
18252223150
19252324150
20212524150
21122120150
22202124150
23202411150
24122011150
25112419150
2619249150
2719910150
28111910150
29242318150
3018238150
311889150
3224189150
3323617150
341767150
351778150
3623178150
DOF#SpecifiedDisplacement
10
20
70
80
130
140
190
200
DOF#Load
9-500
16-500
18-500
21500
MAT#EPNUCTE
130e60.250
(三)运算结果
OutputforInputDatafromfileybx.txt
YangBoxing
PlaneStressAnalysis
Node#X-DisplY-Displ
1-3.6457E-011-4.5660E-011
2-1.2235E-006-3.7328E-006
3-1.0714E-006-4.8037E-006
45.5811E-012-5.2663E-011
5-4.3744E-006-3.4756E-006
61.1298E-006-3.9803E-006
7-2.0895E-011-6.7977E-011
85.6666E-007-8.0484E-006
91.7282E-006-6.9774E-006
105.1771E-011-6.0974E-011
113.4706E-006-2.4557E-006
12-2.2592E-007-1.9510E-006
13-1.4587E-007-2.2104E-006
14-8.6656E-007-4.3286E-006
15-2.2067E-006-3.5616E-006
16-9.6315E-007-3.7692E-006
171.4431E-006-4.3252E-006
188.6656E-007-6.2549E-006
199.0951E-007-2.9741E-006
209.6315E-007-3.5347E-006
212.1868E-008-3.8267E-006
22-1.5185E-006-4.1819E-006
238.2454E-007-4.8759E-006
246.7212E-007-4.5207E-006
251.3818E-021-4.1589E-006
DOF#Reaction
11.6041E+002
22.0090E+002
7-2.4557E+001
82.3172E+002
139.1939E+001
142.9910E+002
19-2.2779E+002
202.6828E+002
ELEM#SXSYTXYS1S2ANGLESX-->S1
1-4.46557E-001-3.18054E-001-3.36112E-001-4.01069E-002-7.24503E-001-3.95889E+001
2-1.77128E-001-6.29567E-001-3.23487E-001-8.60823E-003-7.98086E-001-2.75171E+001
3-2.92511E-002-4.14355E-001-2.14560E-0016.64891E-002-5.10095E-001-2.40472E+001
4-2.98680E-001-1.02842E-001-2.27186E-0014.66284E-002-4.48150E-001-3.33418E+001
5-1.77582E-001-7.25672E-0021.77172E-002-6.96587E-002-1.80490E-001-1.70677E+002
63.90250E-002-2.64533E-002-6.10991E-0027.56036E-002-6.30319E-002-3.09080E+001
7-2.24431E-0011.30444E-001-9.30665E-0021.53370E-001-2.47356E-001-1.38386E+001
8-4.41038E-0018.43304E-002-1.42503E-0028.47166E-002-4.41424E-001-1.55259E+000
9-5.33765E-0015.31106E-0021.69834E-0019.87143E-002-5.79369E-001-1.64969E+002
101.57292E-001-6.56500E-0011.75399E-0011.93487E-001-6.92695E-0011.16596E+001
11-2.65574E-001-1.10905E+000-8.72260E-002-2.56649E-001-1.11798E+000-5.84271E+000
12-9.56632E-001-3.99440E-001-9.27918E-002-3.84394E-001-9.71679E-001-9.21067E+000
13-9.04363E-001-1.90363E-0015.60759E-0011.17392E-001-1.21212E+000-1.51241E+002
14-4.62245E-001-2.66978E-0016.70410E-0013.12871E-001-1.04209E+000-1.39143E+002
15-7.73772E-003-3.97276E-0015.73147E-0014.02830E-001-8.07844E-0013.56155E+001
16-4.49856E-001-3.20661E-0014.63496E-0018.27173E-002-8.53235E-001-1.38967E+00217-5.17669E-001-2.22195E-0011.36976E-001-1.68466E-001-5.71398E-001-1.58582E+002
18-2.77597E-001-2.77597E-0011.92377E-001-8.52197E-002-4.69974E-001-1.35000E+002
19-3.75242E-002-3.32998E-0011.36976E-0011.62048E-002-3.86727E-0012.14177E+001
20-2.77597E-001-2.77597E-0018.15743E-002-1.96022E-001-3.59171E-001-1.35000E+002
21-2.40409E-002-3.93514E-0013.05586E-002-2.15305E-002-3.96025E-0014.69633E+000
22-4.49856E-001-3.20661E-001-7.53301E-002-2.86024E-001-4.84493E-001-2.46931E+001
23-8.88060E-001-1.94125E-0011.81701E-002-1.93650E-001-8.88535E-001-1.78501E+002
24-4.62245E-001-2.66978E-0011.24059E-001-2.06741E-001-5.22481E-001-1.54101E+002
25-8.13238E-0011.05162E-001-5.26633E-0013.44680E-001-1.05276E+000-2.44565E+001
26-1.05128E-002-7.39647E-001-5.39258E-0012.75849E-001-1.02601E+000-2.79696E+001
274.70674E-001-1.91125E-001-8.48171E-0011.05021E+000-7.70659E-001-3.43438E+001
28-3.32051E-0016.53684E-001-8.35546E-0011.13090E+000-8.09263E-001-2.97324E+001
29-2.00285E-001-9.84042E-001-1.42503E-002-2.00026E-001-9.84301E-001-1.04129E+000
30-3.63209E-001-1.04254E+000-8.06780E-002-3.53759E-001-1.05199E+000-6.68065E+000
31-5.72981E-001-8.98036E-001-6.10991E-002-5.61876E-001-9.09141E-001-1.03014E+001
32-4.10057E-001-8.39533E-0015.32867E-003-4.09991E-001-8.39599E-0017.10744E-001
331.14143E-0019.02478E-0022.19281E-0013.21802E-001-1.17411E-0014.34406E+001
34-2.43604E-0011.13317E+0004.24833E-0011.25371E+000-3.64142E-001-1.64160E+002
35-1.33175E-0011.47321E-0016.87458E-0017.08691E-001-6.94545E-001-1.40765E+002
362.24573E-001-8.95599E-0014.81906E-0014.03357E-001-1.07438E+0002.03546E+001
二.桁架结构
桁架如下图,水平链杆的长度为1000mm,9号和13号杆的长度为1000mm,11号杆的长度为2000mm,在结点1,8分别采用固定铰支座、可动铰支座。
在结点2,5,6施加10000N的竖向作用力,然后分析桁架应力的变化。
先将桁架结构分成13个单元,分别编上号码。
在记事本文件以一定的格式写入代码后,运用MATLAB软件进行应力分析。
(一)桁架计算图示
(二)计算代码
truss
Y.B.X
NNNENMNDIMNENNDN
8131222
NDNLNDPC
330
NODEXY
100
210001000
310000
420000
520002000
630001000
730000
840000
单元结点1结点2材料面积温度
11213140
22513140
35613140
46813140
57813140
64713140
73413140
81313140
93213140
102413140
114513140
124613140
136713140
DOF#SPEDIS
10
20
160
DOF#LOAD
4-10000
10-10000
12-10000
MATEEPNUCTE
12.5e50.270
(三)运算结果
OutputforInputDatafromfiletruss.txt
Y.B.X
Node#X-DisplY-Displ
1-8.5592E-022-7.0586E-006
27.7979E-001-1.3203E+000
31.9108E-001-1.3203E+000
43.8217E-001-1.5377E+000
53.8217E-001-1.2829E+000
6-1.5455E-002-1.3203E+000
75.7325E-001-1.3203E+000
87.6433E-001-7.0586E-006
Elem#Stress
1-6.7558E+001
2-4.5039E+001
3-4.5039E+001
4-6.7558E+001
54.7771E+001
64.7771E+001
74.7771E+001
84.7771E+001
95.5511E-014
10-2.2519E+001
113.1847E+001
12-2.2519E+001
13-5.5511E-014
DOF#Reaction
11.8189E-012
21.5000E+004
161.5000E+004
三.刚架结构
刚架计算简图如下图,在结点4,8,12采用固定支座。
在结点2,5,10施加3000000N的竖向作用力。
然后分析刚架应力的变化。
先将刚架结构分成20个单元,分别编上号码。
在记事本文件以一定的格式写入代码后,运用MATLAB软件进行应力分析。
(一)刚架计算图示
(二)计算代码
frame
Y.B.X
NNNENMNDIMNENNDN
13201223
NDNLNMPC
930
NODE#XY
100
220001000
320000
42000-2000
530000
640002000
740004000
84000-2000
950000
1060001000
1160000
126000-2000
1380000
ELEM#NODE1NODE2MATERAREAINERTEMP
1121314600
2231314600
3341314600
4131314600
5351314600
6571314600
7261314600
8561314600
9671314600
10781314600
11791314600
12691314600
139101314600
1410111314600
1511121314600
169111314600
176101314600
1810131314600
1911131314600
20251314600
DOF#SPEDIS
100
110
120
220
230
240
340
350
360
DOF#LOAD
5-3000000
17-3000000
29-3000000
MATE#EPNUCTE
12.4e50.270
(三)运算结果
OutputforInputDatafromfileframe1.txt
Y.B.X
NODE#X-Displ.Y-Displ.Z-Rot.
1-1.9849E+0027.5635E+001-8.7215E-002
2-1.0212E+002-1.1711E+002-1.0795E-001
3-1.9849E+002-7.8075E+001-6.2164E-002
4-3.2582E-009-1.7024E-0032.9991E-006
5-1.9849E+002-2.1203E+002-1.3286E-001
6-8.5218E-008-3.1847E+0024.1572E-013
7-8.5218E-008-2.4812E+0023.4927E-012
8-3.4602E-020-1.8035E-0031.0866E-016
91.9849E+002-2.1203E+0021.3286E-001
101.0212E+002-1.1711E+0021.0795E-001
111.9849E+002-7.8075E+0016.2164E-002
123.2582E-009-1.7024E-003-2.9991E-006
131.9849E+0027.5635E+0018.7215E-002
DOF#Reaction
105.6301E+000
112.9418E+006
12-5.1825E+003
225.9792E-011
233.1164E+006
24-1.8776E-007
34-5.6301E+000
352.9418E+006
365.1825E+003
MemberEnd-Forces
Member#1
-1.2563E-001-4.1764E-0028.6827E+001
1.2563E-0014.1764E-002-1.8021E+002
Member#2
2.9418E+0061.9556E+0003.1849E+002
-2.9418E+006-1.9556E+0001.6371E+003
Member#3
2.9418E+006-5.6301E+000-6.0777E+003
-2.9418E+0065.6301E+000-5.1825E+003
Member#4
9.3690E-0029.3539E-002-8.6827E+001
-9.3690E-002-9.3539E-0022.7390E+002
Member#5
7.6794E+0006.2976E+0004.1667E+003
-7.6794E+000-6.2976E+0002.1308E+003
Member#6
-2.3995E+005-1.7891E-001-8.3283E+002
2.3995E+0051.7891E-0019.5172E+001
Member#7
-4.3373E+0041.6241E+0001.1206E+003
4.3373E+004-1.6241E+0002.5109E+003
Member#8
2.1689E+0051.1839E+0004.6809E+002
-2.1689E+005-1.1839E+0002.1792E+003
Member#9
-2.6508E+0068.4414E-0116.2260E-008
2.6508E+006-8.4414E-0111.0657E-007
Member#10
3.1164E+006-5.9792E-011-1.7099E-007
-3.1164E+0065.9792E-011-1.8776E