1-学习tecplot360
FETRIANGLE(3节点三角形), FEQUADRILATERAL(4节点四边形),FETETRAHEDRON(4节点四面体), FEBRICK(8节点六面体)
参考:https://wenku.baidu.com/view/70b794168e9951e79a892721.html?from=search
https://wenku.baidu.com/view/ab0a4559a5e9856a561260b6.html
http://www.doc88.com/p-618423100007.html
1.绘制二维图形xy线型图：
新建文本文档，输入下面代码，打开tecplot360-file--load data files--选择tecplot data loader --选择保存的刚才输入文本文档并保存的代码。
title="a"
variables=x,y
zone t="line1"
i=,j=,f=point
上述文件是一个顺序文件，包括了标题，变量，域定义。描述的是6个点相连的情况。
----------------
VARIABLES = "X","Y"
ZONE I=,J=, F=POINT
-------------------------------------
title="a"
variables=x,y
zone t="line1"
i=,j=,f=point zone t="line2"
改变i，j没变化：
title="saledcar"
variables=x,y
zone t="line1"
i=,j=,f=point
VARIABLES = "X", "Y", "Intensity", "Pressure"
ZONE I=, J=, F=POINT
2.绘制单元格式图：
TITLE = "Example: 2D Finite-Element Data"
VARIABLES = "X", "Y", "P", "T"
ZONE N=, E=, F=FEPOINT, ET=QUADRILATERAL
0.0 1.0 100.0 1.6
1.0 1.0 150.0 1.5
3.0 1.0 300.0 2.0
0.0 0.0 50.0 1.0
1.0 0.0 100.0 1.4
3.0 0.0 200.0 2.2
4.0 0.0 400.0 3.0
2.0 2.0 280.0 1.9
通过实验可知，二维平面图形，单元的节点可以顺时针也可以逆时针，无所谓。
但不能单元内节点乱放，顺时针或逆时针都行，但不能跳过节点最后再补：
------------------------------
VARIABLES = "X", "Y"
ZONE N=, E=, F=FEPOINT, ET=TRIANGLE
1.0 1.0
2.0 3.0
2.5 1.0
3.5 5.0
4.0 1.0
-------------------
TITLE="DUPLICATE IJ FELINESEG, FETRIANGLE(3节点三角形),FEQUADRILATERAL(4节点四边形),FETETRAHEDRON(4节点四面体), FEBRICK(8节点六面体)"
VARIABLES=X,Y,Z
ZONE I=, J=, F=POINT
,,
,,
,,
,,
ZONE I=, J=, F=POINT, D=(,)
-----------------
TITLE = "Example: Variable and Connectivity List Sharing"
VARIABLES = "X", "Y", "P"
ZONE T="P_1", N=, E=, DATAPACKING=POINT, ZONETYPE=FETRIANGLE
-1.0 0.0
0.0 0.0
1.0 0.0
-0.5 0.8
0.5 0.8
0.0 1.6 ZONE T="P_2", N=, E=, DATAPACKING=POINT, ZONETYPE=FETRIANGLE, VARSHARELIST= ([, ]=), CONNECTIVITYSHAREZONE = ZONE T="P_3", N=, E=, DATAPACKING=POINT, ZONETYPE=FETRIANGLE, VARSHARELIST= ([, ]=), CONNECTIVITYSHAREZONE =
title = "example: variable and connectivity list sharing"
variables = "x", "y", "p"
zone t="p_1", n=, e=, datapacking=point, zonetype=fetriangle
-1.0 0.0
0.0 0.0
1.0 0.0
-0.5 0.8
0.5 0.8
0.0 1.6 zone t="p_2", n=, e=, datapacking=point, zonetype=fetriangle, varsharelist= ([, ]=), connectivitysharezone = zone t="p_3", n=, e=, datapacking=point, zonetype=fetriangle, varsharelist= ([, ]=), connectivitysharezone =
tecplot读入代码，小写也无所谓
title=" quad2"
variables=x,y
ZONE N=,E=,F=FEPOINT,ET=QUADRILATERAL
0.5 1.0
0.5 1.5
0.5 2.0
1.0 1.0
1.0 1.5
1.0 2.0
TITLE = "2D-quad"
VARIABLES = "X", "Y", "Z"
Zone I=,j=,f=point
2.000000 5.000000 -19.178485
4.000000 7.000000 26.279464
6.000000 9.000000 24.727109
8.000000 11.000000 -79.999217
10.000000 13.000000 42.016704
2.000000 8.000000 19.787165
4.000000 10.0000000 -21.760844
6.000000 12.000000 -32.194375
8.000000 14.000000 79.248588
10.000000 16.000000 -28.790332
2.000000 11.000000 -19.999804
4.0000000 13.000000 16.806681
6.000000 15.000000 39.017270
8.000000 17.000000 -76.911799
10.000000 19.000000 14.987721
2.000000 14.000000 19.812147
4.000000 16.000000 -11.516133
6.000000 18.000000 -45.059235
8.000000 20.000000 73.035620
10.000000 22.000000 -0.885131
还可以拓展：
比如，我节点上存在不止一个量，那么应该如何写呢，如下：
TITLE = "2D-quad"
VARIABLES = "X", "Y", "Z1", "Z2", "Z3"
Zone I=,j=,f=point
-19.178485 2.5
26.279464 1.75
24.727109 1.5
-79.999217 1.375
42.016704 1.3
19.787165
-21.760844 2.5
-32.194375
79.248588 1.75
-28.790332 1.6
-19.999804 5.5
16.806681 3.25
39.01727 2.5
-76.911799 2.125
14.987721 1.9
19.812147
-11.516133
-45.059235
73.03562 2.5
-0.885131 2.2
当然，添加上k=1这个参数也是正确的，如下第三行：
TITLE = "2D-quad"
VARIABLES = "X", "Y", "Z1", "Z2", "Z3"
Zone I=,j=,k=,f=point
-19.178485 2.5
26.279464 1.75
24.727109 1.5
-79.999217 1.375
42.016704 1.3
19.787165
-21.760844 2.5
-32.194375
79.248588 1.75
-28.790332 1.6
-19.999804 5.5
16.806681 3.25
39.01727 2.5
-76.911799 2.125
14.987721 1.9
19.812147
-11.516133
-45.059235
73.03562 2.5
-0.885131 2.2
拓展，比如我要现实一个区域两个不同时刻的值。在有限元二位计算中经常出现用不同时步让显示节点位移或增量位移等情况，就可以用这个扩展：
TITLE = "2D-quad1"
VARIABLES = "X", "Y", "Z1", "Z2", "Z3"
Zone I=,j=,k=,f=point
-19.178485 2.5
26.279464 1.75
24.727109 1.5
-79.999217 1.375
42.016704 1.3
19.787165
-21.760844 2.5
-32.194375
79.248588 1.75
-28.790332 1.6
-19.999804 5.5
16.806681 3.25
39.01727 2.5
-76.911799 2.125
14.987721 1.9
19.812147
-11.516133
-45.059235
73.03562 2.5
-0.885131 2.2
TITLE = "2D-quad2"
VARIABLES = "X", "Y", "Z1", "Z2", "Z3"
Zone I=,j=,k=,f=point
-19.178485
26.279464
24.727109
-79.999217
42.016704
19.787165
-21.760844
-32.194375
79.248588
-28.790332
-19.999804
16.806681
39.01727
-76.911799
14.987721
19.812147
-11.516133
-45.059235
73.03562
-0.885131
TITLE = "2D-quad1"
VARIABLES = "X", "Y", "Z1", "x*y", "y/x"
Zone t="zone-t1", I=,j=,k=,f=point
-19.178485 2.5
26.279464 1.75
24.727109 1.5
-79.999217 1.375
42.016704 1.3
19.787165
-21.760844 2.5
-32.194375
79.248588 1.75
-28.790332 1.6
-19.999804 5.5
16.806681 3.25
39.01727 2.5
-76.911799 2.125
14.987721 1.9
19.812147
-11.516133
-45.059235
73.03562 2.5
-0.885131 2.2
VARIABLES = "X", "Y", "Z1", "x*x", "y*y"
Zone t="zone-t2", I=,j=,k=,f=point
-19.178485
26.279464
24.727109
-79.999217
42.016704
19.787165
-21.760844
-32.194375
79.248588
-28.790332
-19.999804
16.806681
39.01727
-76.911799
14.987721
19.812147
-11.516133
-45.059235
73.03562
-0.885131
上面代码是顺序数据结果中两种不同的数
据排布方法中的一种，把“f=point” 改成“f=block”,那
么Tecplot会先期待所有关于x的值，接着是
y,z。
TITLE = "same mesh"
variables="x","y","z"
zone I=,j=,f=block
2.000000 4.000000 6.000000 8.000000 10.000000
2.000000 4.000000 6.000000 8.000000 10.00000
2.000000 4.000000 6.000000 8.000000 10.000000
2.000000 4.000000 6.000000 8.000000 10.000000
5.000000 7.000000 9.000000 11.000000 13.000000
8.000000 10.000000 12.000000 14.000000 16.000000
11.000000 13.000000 15.000000 17.000000 19.000000
14.000000 16.000000 18.000000 20.000000 22.000000
-19.178485 26.279464 24.727109 -79.999217 42.016704
19.787165 -21.760844 -32.194375 79.248588 -28.790332
-19.999804 16.806681 39.017270 -76.911799 14.987721
19.812147 -11.516133 -45.059235 73.035620 -0.885131
Title="finite-element data for brick"
Variables="x","y","z"
Zone n=,e=,f=fepoint,et=brick
. . .
. 1.000000 .
. 2.000000 .
. . 1.000000
. 1.000000 1.000000
. 2.000000 1.000000
. . 2.000000
. 1.000000 2.000000
. 2.000000 2.000000 3.000000 . .
3.000000 1.000000 .
3.000000 2.000000 .
2.500000 . 1.000000
2.500000 1.000000 1.000000
2.500000 2.000000 1.000000
2.000000 . 2.000000
2.000000 1.000000 2.000000
2.000000 2.000000 2.000000 6.000000 . .
6.000000 1.000000 .
6.000000 2.000000 .
5.000000 . 1.000000
5.000000 1.000000 1.000000
5.000000 2.000000 1.000000
4.000000 . 2.000000
4.000000 1.000000 2.000000
4.000000 2.000000 2.000000 8.000000 . .
8.000000 1.000000 .
8.000000 2.000000 .
7.500000 . 1.000000
7.500000 1.000000 1.000000
7.500000 2.000000 1.000000
7.000000 . 2.000000
7.000000 1.000000 2.000000
7.000000 2.000000 2.000000 10.000000 . .
10.000000 1.000000 .
10.000000 2.000000 .
10.000000 . 1.000000
10.000000 1.000000 1.000000
10.000000 2.000000 1.000000
10.000000 . 2.000000
10.000000 1.000000 2.000000
10.000000 2.000000 2.000000
文本自上而下分别是不同节点（1,2,3,4...45，只不过节点编号在坐标前面没有显示）的（x,y,z）坐标，之后是不同单元（1,2,3,4...16，也没有在节点编号前显示）由哪些节点编号的节点组成（这些节点组成单元是有顺序的，不能打乱同行的节点编号），但不同行节点编号可以整行变换，也就是单元可以整体换在文本中位置，但节点在单元内的位置不能换。
比如：
和下面的整行交换后效果一样： 但下面节点编号交换就不行：
Title="finite-element,data,for,brick"
Variables="x","y","z"
Zone,n=,e=,f=fepoint,et=brick
.,.,.
.,1.000000,.
.,2.000000,.
.,.,1.000000
.,1.000000,1.000000
.,2.000000,1.000000
.,.,2.000000
.,1.000000,2.000000
.,2.000000,2.000000 3.000000,.,.
3.000000,1.000000,.
3.000000,2.000000,.
2.500000,.,1.000000
2.500000,1.000000,1.000000
2.500000,2.000000,1.000000
2.000000,.,2.000000
2.000000,1.000000,2.000000
2.000000,2.000000,2.000000 6.000000,.,.
6.000000,1.000000,.
6.000000,2.000000,.
5.000000,.,1.000000
5.000000,1.000000,1.000000
5.000000,2.000000,1.000000
4.000000,.,2.000000
4.000000,1.000000,2.000000
4.000000,2.000000,2.000000 8.000000,.,.
8.000000,1.000000,.
8.000000,2.000000,.
7.500000,.,1.000000
7.500000,1.000000,1.000000
7.500000,2.000000,1.000000
7.000000,.,2.000000
7.000000,1.000000,2.000000
7.000000,2.000000,2.000000 10.000000,.,.
10.000000,1.000000,.
10.000000,2.000000,.
10.000000,.,1.000000
10.000000,1.000000,1.000000
10.000000,2.000000,1.000000
10.000000,.,2.000000
10.000000,1.000000,2.000000
10.000000,2.000000,2.000000 ,,,,,,,
,,,,,,, ,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
,,,,,,,
上述代码也可以用逗号分隔代替空格分隔
Title= "sample finite-element data "
Variables="x","y","a","b"
Zone n=,e=, f=fepoint ,et=triangle
0.0 0.0 1.0 2.0
-1.0 -1.0 0.0 2.2
-1.0 1.0 0.0 3.0
1.0 1.0 0.0 3.4
1.0 -1.0 0.0 .
实战出图：
title="Feadam 2d model post-process"
variables= "X", "Y",DELTA-X DELTA-Y X-DISP Y-DISP TOTAL
ZONE t="LAYER NUMBER = 1" ,N=, E=, F=FEPOINT, ET=QUADRILATERAL,VARLOCATION=([-]=CELLCENTERED)
0.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
50.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
80.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
100.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
120.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
140.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
160.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
180.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
200.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
0.000 15.000 0.0000 0.0012 0.0000 0.0012 0.0012
50.000 15.000 0.0126 0.0005 -0.0126 0.0005 0.0126
80.000 15.000 0.0343 0.0039 -0.0343 0.0039 0.0346
100.000 15.000 0.0722 0.0024 -0.0722 0.0024 0.0722
120.000 15.000 0.0779 -0.0763 -0.0779 -0.0763 0.1090
140.000 15.000 0.0344 -0.0794 -0.0344 -0.0794 0.0865
160.000 15.000 0.0157 -0.0714 -0.0157 -0.0714 0.0731
180.000 15.000 0.0060 -0.0716 -0.0060 -0.0716 0.0718
200.000 15.000 0.0000 -0.0707 0.0000 -0.0707 0.0707
0.000 25.000 0.0000 0.0027 0.0000 0.0027 0.0027
50.000 25.000 0.0162 0.0031 -0.0162 0.0031 0.0165
80.000 25.000 0.0450 0.0109 -0.0450 0.0109 0.0463
100.000 25.000 0.0750 0.0125 -0.0750 0.0125 0.0761
120.000 25.000 0.0773 -0.1447 -0.0773 -0.1447 0.1640
140.000 25.000 0.0539 -0.1422 -0.0539 -0.1422 0.1521
160.000 25.000 0.0225 -0.1310 -0.0225 -0.1310 0.1329
180.000 25.000 0.0076 -0.1254 -0.0076 -0.1254 0.1256
200.000 25.000 0.0000 -0.1248 0.0000 -0.1248 0.1248
120.000 35.000 0.0000 0.0000 0.0000 0.0000 0.0000
140.000 35.000 0.0000 0.0000 0.0000 0.0000 0.0000
160.000 35.000 0.0000 0.0000 0.0000 0.0000 0.0000
180.000 35.000 0.0000 0.0000 0.0000 0.0000 0.0000
200.000 35.000 0.0000 0.0000 0.0000 0.0000 0.0000
TITLE = "feadam 2d model post-process"
VARIABLES = "x"
"y"
"delta-x"
"delta-y"
"x-disp"
"y-disp"
"total"
ELAS-MOD BULK-MOD POIS EPS-X EPS-Y GAM-XY EPS- EPS- GAMMAX EPS-V
SIG-X SIG-Y TAU-XY SIG- SIG- TAU-MAX THETA SIG1/SIG3 TAUXY/SIGY SLCRIT SLPRES ZONE T="LOAD CASE AFTER CONSTRUCTION 1"
STRANDID=, SOLUTIONTIME=
Nodes=, Elements=, ZONETYPE=FEQuadrilateral
DATAPACKING=BLOCK
varlocation=([-]=cellcentered) 0.000000000E+000 5.000000000E+001 8.000000000E+001 1.000000000E+002 1.200000000E+002
1.400000000E+002 1.600000000E+002 1.800000000E+002 2.000000000E+002 0.000000000E+000
5.000000000E+001 8.000000000E+001 1.000000000E+002 1.200000000E+002 1.400000000E+002
1.600000000E+002 1.800000000E+002 2.000000000E+002 0.000000000E+000 5.000000000E+001
8.000000000E+001 1.000000000E+002 1.200000000E+002 1.400000000E+002 1.600000000E+002
1.800000000E+002 2.000000000E+002 1.200000000E+002 1.400000000E+002 1.600000000E+002
1.800000000E+002 2.000000000E+002 1.400000000E+002 1.600000000E+002 1.800000000E+002
2.000000000E+002 1.600000000E+002 1.800000000E+002 2.000000000E+002
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 1.500000000E+001
1.500000000E+001 1.500000000E+001 1.500000000E+001 1.500000000E+001 1.500000000E+001
1.500000000E+001 1.500000000E+001 1.500000000E+001 2.500000000E+001 2.500000000E+001
2.500000000E+001 2.500000000E+001 2.500000000E+001 2.500000000E+001 2.500000000E+001
2.500000000E+001 2.500000000E+001 3.500000000E+001 3.500000000E+001 3.500000000E+001
3.500000000E+001 3.500000000E+001 4.500000000E+001 4.500000000E+001 4.500000000E+001
4.500000000E+001 5.500000000E+001 5.500000000E+001 5.500000000E+001
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
-3.100000089E-003 -1.000000047E-003 1.200000057E-003 1.000000047E-003 -4.000000190E-003
-7.600000128E-003 -5.599999800E-003 0.000000000E+000 0.000000000E+000 -1.000000047E-003
-2.099999925E-003 -5.700000096E-003 -4.800000228E-003 -8.999999613E-003 -1.119999960E-002
-7.799999788E-003 0.000000000E+000 -1.319999993E-002 -9.800000116E-003 -1.009999961E-002
-6.800000090E-003 0.000000000E+000 -1.030000020E-002 -6.500000134E-003 -3.400000045E-003
0.000000000E+000 3.000000142E-004 1.799999969E-003 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 -1.090000011E-002
-2.040000074E-002 -2.060000040E-002 -1.810000092E-002 -9.499999695E-003 -5.599999800E-003
-8.100000210E-003 -1.229999959E-002 -1.370000001E-002 -1.979999989E-002 -3.500000015E-002
-3.180000186E-002 -3.200000152E-002 -1.549999975E-002 -7.899999619E-003 -1.400000043E-002
-2.250000089E-002 -2.559999935E-002 -1.830000058E-002 -9.800000116E-003 -1.850000024E-002
-3.209999949E-002 -3.550000116E-002 -1.279999968E-002 -2.199999988E-002 -3.990000114E-002
-4.369999841E-002 -2.500000037E-002 -4.820000008E-002 -4.769999906E-002
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
-2.730000019E-002 -6.800000370E-002 -1.419000030E-001 -2.045000046E-001 -1.645999998E-001
-1.076000035E-001 -4.820000008E-002 0.000000000E+000 0.000000000E+000 -3.099999949E-002
-9.170000255E-002 -1.972000003E-001 -2.175000012E-001 -2.116000056E-001 -1.356000006E-001
-6.400000304E-002 0.000000000E+000 -1.168000028E-001 -1.033999994E-001 -1.010999978E-001
-5.330000073E-002 0.000000000E+000 -3.519999981E-002 -2.329999954E-002 -1.899999939E-002
0.000000000E+000 3.000000142E-004 1.799999969E-003 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 -8.899999782E-003
-1.950000040E-002 -1.360000018E-002 -3.999999899E-004 -9.849999845E-002 -1.606000066E-001
-1.924999952E-001 -2.075999975E-001 -2.075999975E-001 -1.480000000E-002 -3.020000085E-002
-8.500000462E-003 2.129999921E-002 -1.761000007E-001 -2.827999890E-001 -3.555000126E-001
-3.693000078E-001 -3.727000058E-001 -3.089999966E-002 -1.738000065E-001 -2.874999940E-001
-3.265999854E-001 -3.264000118E-001 -5.050000176E-002 -1.604000032E-001 -2.171999961E-001
-2.281000018E-001 -2.500000037E-002 -4.820000008E-002 -4.769999906E-002
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 8.899999782E-003
3.350000083E-002 6.939999759E-002 1.419000030E-001 2.268999964E-001 2.300000042E-001
2.205000073E-001 2.131000012E-001 2.075999975E-001 1.480000000E-002 4.329999909E-002
9.210000187E-002 1.984000057E-001 2.799000144E-001 3.531999886E-001 3.804999888E-001
3.747999966E-001 3.727000058E-001 1.208000034E-001 2.022999972E-001 3.048000038E-001
3.309000134E-001 3.264000118E-001 6.150000170E-002 1.620000005E-001 2.180999964E-001
2.281000018E-001 2.500000037E-002 4.820000008E-002 4.769999906E-002 60.4 56.7 66.4 66.6 72.2 79.6 85.7 53.9 88.8 78.6 73.2 65.5 73.2 354.2 188.7 159.2 113.1 118.4 129.6 160.5 174.6 151.2 124.8 177.8 184.7
94.3 96.2 97.8 104.4 110.9 117.5 122.8 79.5 88.9 88.4 107.6 111.2 115.8 117.4 315.8 168.3 141.9 108.5 115.6 143.1 155.7 134.8 111.3 158.5 164.7
0.399 0.395 0.403 0.394 0.4 0.398 0.39 0.384 0.387 0.333 0.352 0.395 0.387 0.402 0.401 0.396 0.313 0.313 0.313 0.326 0.334 0.313 0.313 0.313 0.313 0.313 0.313 0.313
0.027 0.068 0.185 0.156 -0.1 -0.143 -0.148 -0.121 0.058 0.169 0.449 0.207 -0.114 -0.333 -0.327 -0.28 0.09 0.011 -0.117 -0.261 -0.274 -0.027 -0.041 -0.079 -0.122 -0.019 -0.012 -0.004
0.094 0.11 0.047 0.33 0.864 1.177 1.334 1.384 0.083 0.028 -0.134 0.28 0.999 1.426 1.624 1.635 -0.006 0.163 0.481 0.728 0.806 0.057 0.171 0.319 0.376 0.03 0.056 0.061
0.101 0.308 0.667 1.4 1.386 0.987 0.557 0.161 0.045 0.091 0.288 1.081 0.722 0.636 0.291 0.087 -0.033 0.242 0.163 0.071 -0.006 -0.073 0.191 0.045 -0.013 -0.022 0.043 -0.018
0.122 0.245 0.456 0.948 1.226 1.341 1.384 1.388 0.096 0.183 0.482 0.785 1.106 1.482 1.634 1.636 0.092 0.23 0.492 0.73 0.806 0.071 0.208 0.32 0.376 0.033 0.063 0.063
-0.066 -0.225 -0.462 -0.462 -0.307 -0.199 -0.125 0.045 0.014 -0.168 -0.298 -0.221 -0.388 -0.338 -0.281 -0.009 -0.056 -0.128 -0.263 -0.274 -0.041 -0.078 -0.08 -0.122 -0.021 -0.018 -0.005
0.122 0.311 0.681 1.41 1.688 1.648 1.583 1.513 0.051 0.168 0.65 1.083 1.327 1.87 1.973 1.917 0.101 0.286 0.62 0.992 1.08 0.112 0.286 0.4 0.499 0.054 0.081 0.068
0.122 0.178 0.232 0.486 0.764 1.035 1.185 1.263 0.142 0.197 0.315 0.487 0.885 1.093 1.296 1.354 0.084 0.174 0.364 0.467 0.532 0.03 0.13 0.24 0.254 0.011 0.045 0.057 0.414 0.482 0.579 0.784 0.958 1.195 1.333 1.418 0.201 0.299 0.468 0.52 0.79 0.891 1.067 1.134 0.381 0.361 0.384 0.294 0.347 0.073 0.238 0.317 0.263 0.066 0.185 0.212
0.749 0.803 0.819 1.159 1.634 2.1 2.374 2.512 0.302 0.337 0.368 0.632 1.26 1.65 2.014 2.116 0.321 0.715 1.289 1.494 1.667 0.231 0.663 1.012 1.035 0.188 0.427 0.454
0.019 0.073 0.154 0.248 0.274 0.237 0.148 0.046 0.008 0.022 0.054 0.163 0.151 0.131 0.069 0.022 0.005 0.161 0.098 0.031 -0.003 -0.003 0.124 0.03 -0.008 0.023 0.029 -0.012
0.75 0.818 0.894 1.283 1.731 2.158 2.395 2.514 0.303 0.347 0.492 0.749 1.304 1.672 2.019 2.117 0.382 0.778 1.3 1.494 1.667 0.231 0.697 1.013 1.035 0.192 0.431 0.455
0.413 0.466 0.504 0.66 0.861 1.136 1.312 1.417 0.201 0.289 0.344 0.404 0.745 0.87 1.062 1.133 0.32 0.299 0.374 0.293 0.347 0.073 0.204 0.316 0.263 0.062 0.181 0.211
0.169 0.176 0.195 0.311 0.435 0.511 0.541 0.549 0.051 0.029 0.074 0.173 0.279 0.401 0.478 0.492 0.031 0.24 0.463 0.601 0.66 0.079 0.246 0.349 0.386 0.065 0.125 0.122
3.254 12.228 26.105 26.451 19.532 13.828 7.935 2.406 4.513 24.436 66.577 35.518 16.37 9.503 4.138 1.288 85.235 21.183 6.088 1.475 -0.14 -0.991 15.153 2.446 -0.596 10.402 6.754 -2.919
1.816 1.755 1.776 1.943 2.01 1.899 1.825 1.775 1.508 1.202 1.428 1.856 1.75 1.922 1.9 1.868 1.193 2.604 3.479 5.104 4.802 3.182 3.412 3.208 3.93 3.107 2.374 2.15
0.025 0.091 0.189 0.214 0.168 0.113 0.062 0.018 0.026 0.065 0.146 0.258 0.12 0.079 0.034 0.01 0.016 0.226 0.076 0.021 -0.002 -0.012 0.187 0.029 -0.008 0.123 0.068 -0.027
0.267 0.259 0.277 0.371 0.411 0.376 0.352 0.334 0.12 0.104 0.199 0.292 0.296 0.37 0.371 0.362 0.057 0.187 0.339 0.473 0.494 0.079 0.211 0.268 0.312 0.065 0.11 0.104
0.264 0.255 0.268 0.351 0.4 0.375 0.352 0.334 0.12 0.057 0.129 0.275 0.288 0.366 0.371 0.362 0.024 0.187 0.339 0.473 0.494 0.079 0.211 0.268 0.312 0.065 0.11 0.104
feadam84计算最终结果
模型节点编号：
单元编号：
整个处理过程说一下；
EXAM TOTAL NUMBER OF ELEMENTS**********
TOTAL NUMBER OF NODES*************
NUMBER OF ELEMENTS IN FOUNDATION**
NUMBER OF NODES IN FOUNDATION*****
NUMBER OF PREEXISTING ELEMENTS****
NUMBER OF PREEXISTING NODES*******
NUMBER OF DIFF. MATERIALS*********
NUMBER OF CONSTRUCTION LAYERS*****
NUMBER OF LOAD CASES************** RESULTS OF THE FOLLOWING LOAD INCREMENTS WILL BE PRINTED EXECUTION STOPS AT THE END OF INCREMENT NO. FINAL RESULTS ARE NOT PUNCHED OUT MATERIAL PROPERTY DATA ATMOSPHERIC PRESSURE= 1.0580 YOUNG'S MODULUS BULK MODULUS
MAT UNIT WT K KUR N RF KB M C PHI DPHI KO 0.0350 120.0 180.0 0.50 0.70 110.00 0.20 0.13 30.00 0.00 0.50
0.0600 400.0 600.0 0.40 0.70 200.00 0.50 0.50 33.00 0.00 0.50 NODAL POINT INPUT DATA NODE NODAL POINT COORDINATES B.C. CODE
NUMBER X-ORD Y-ORD XX YY 0.000 0.000
50.000 0.000
80.000 0.000
100.000 0.000
120.000 0.000
140.000 0.000
160.000 0.000
180.000 0.000
200.000 0.000
0.000 15.000
50.000 15.000
80.000 15.000
100.000 15.000
120.000 15.000
140.000 15.000
160.000 15.000
180.000 15.000
200.000 15.000
0.000 25.000
50.000 25.000
80.000 25.000
100.000 25.000
120.000 25.000
140.000 25.000
160.000 25.000
180.000 25.000
200.000 25.000
120.000 35.000
140.000 35.000
160.000 35.000
180.000 35.000
200.000 35.000
140.000 45.000
160.000 45.000
180.000 45.000
200.000 45.000
160.000 55.000
180.000 55.000
200.000 55.000 FOUR NODES SOLID ELEMENT DATA ELE CONNECTED NODES MATL ELEMENT CENTER COORDINATES
NO. I J K L NO. X-ORD Y-ORD 25.000 7.500
65.000 7.500
90.000 7.500
110.000 7.500
130.000 7.500
150.000 7.500
170.000 7.500
190.000 7.500
25.000 20.000
65.000 20.000
90.000 20.000
110.000 20.000
130.000 20.000
150.000 20.000
170.000 20.000
190.000 20.000
115.000 30.000
130.000 30.000
150.000 30.000
170.000 30.000
190.000 30.000
135.000 40.000
150.000 40.000
170.000 40.000
190.000 40.000
155.000 50.000
170.000 50.000
190.000 50.000 EQUATION NUMBERS N X Y BAND WIDTH************************
NUMBER OF EQUATIONS***************
NUMBER OF EQUATIONS IN BLOCK****** CONSTRUCTION LAYER INFORMATION LAYER ADDED ELEMENTS ADDED NODES NODES OF HUMPED SURFACE FOUNDATION PART INFORMATION NUMBER OF LAYERS IN FOUNDATION****
ELEVATION OF RIGID BOUNDARY******* 0.000 LAYER MAT. NO. INCLUSIVE ELEMENTS ELEVATION 15.000
25.000 INITIAL VALUES IN ELEMENTS ELE X-ORD Y-ORD ELAS MOD BULK MOD SIG-X SIG-Y TAU-XY SLCRIT 25.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
65.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
90.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
110.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
130.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
150.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
170.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
190.000 7.500 43.5 90.8 0.306 0.612 0.000 0.343
25.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
65.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
90.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
110.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
130.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
150.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
170.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
190.000 20.000 29.7 70.7 0.087 0.175 0.000 0.166
115.000 30.000 123.0 109.7 0.075 0.150 0.034 0.000
130.000 30.000 139.3 124.2 0.150 0.300 0.000 0.037
150.000 30.000 139.3 124.2 0.150 0.300 0.000 0.037
170.000 30.000 139.3 124.2 0.150 0.300 0.000 0.037
190.000 30.000 139.3 124.2 0.150 0.300 0.000 0.037
135.000 40.000 123.0 109.7 0.075 0.150 0.034 0.026
150.000 40.000 139.3 124.2 0.150 0.300 0.000 0.037
170.000 40.000 139.3 124.2 0.150 0.300 0.000 0.037
190.000 40.000 139.3 124.2 0.150 0.300 0.000 0.037
155.000 50.000 123.0 109.7 0.075 0.150 0.034 0.026
170.000 50.000 139.3 124.2 0.150 0.300 0.000 0.037
190.000 50.000 139.3 124.2 0.150 0.300 0.000 0.037 EXAM ********************************************************
********************************************************
* *
* LAYER NUMBER***************************** *
* *
********************************************************
******************************************************** ADDED ELEMENTS******************** THRU
ADDED NODAL POINTS**************** THRU
NODAL POINTS OF HUMPED SURFACE**** BAND WIDTH************************
TOTAL NUMBER OF EQUATIONS*********
NUMBER OF EQUATIONS IN BLOCK******
NUMBER OF BLOCKS****************** NODAL POINT FORCES (WEIGHTS OF ADDED ELEMENTS) NP X-FORCE Y-FORCE 0.000 -2.000
0.000 -5.000
0.000 -6.000
0.000 -6.000
0.000 -6.000
0.000 -3.000
0.000 -5.000
0.000 -6.000
0.000 -6.000
0.000 -6.000
0.000 -3.000 LAYER NUMBER = ITERATION =
*********************************************************** NP DELTA-X DELTA-Y X-DISP Y-DISP TOTAL NP 0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0012 0.0000 0.0012 0.0012
-0.0126 0.0005 -0.0126 0.0005 0.0126
-0.0343 0.0039 -0.0343 0.0039 0.0346
-0.0722 0.0024 -0.0722 0.0024 0.0722
-0.0779 -0.0763 -0.0779 -0.0763 0.1090
-0.0344 -0.0794 -0.0344 -0.0794 0.0865
-0.0157 -0.0714 -0.0157 -0.0714 0.0731
-0.0060 -0.0716 -0.0060 -0.0716 0.0718
0.0000 -0.0707 0.0000 -0.0707 0.0707
0.0000 0.0027 0.0000 0.0027 0.0027
-0.0162 0.0031 -0.0162 0.0031 0.0165
-0.0450 0.0109 -0.0450 0.0109 0.0463
-0.0750 0.0125 -0.0750 0.0125 0.0761
-0.0773 -0.1447 -0.0773 -0.1447 0.1640
-0.0539 -0.1422 -0.0539 -0.1422 0.1521
-0.0225 -0.1310 -0.0225 -0.1310 0.1329
-0.0076 -0.1254 -0.0076 -0.1254 0.1256
0.0000 -0.1248 0.0000 -0.1248 0.1248
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000 MODULUS AND POISSON'S RATIO VALUES BASED ON AVERAGE STRESSES DURING THE INCREMENT
STRAINS FOR FINAL CONDITION AT END OF INCREMENT ELE ELAS MOD BULK MOD POIS EPS-X EPS-Y GAM-XY EPS- EPS- GAMMAX EPS-V ELE 48.0 91.1 0.412 0.013 -0.006 0.043 0.027 -0.020 0.046 0.007
62.1 91.8 0.387 0.036 -0.015 0.151 0.090 -0.069 0.159 0.021
74.4 93.8 0.368 0.095 -0.021 0.359 0.225 -0.152 0.377 0.074
49.0 96.0 0.415 0.014 0.246 0.697 0.498 -0.237 0.734 0.261
51.3 98.5 0.413 -0.109 0.519 0.382 0.572 -0.162 0.735 0.410
56.5 100.2 0.406 -0.047 0.502 0.147 0.512 -0.056 0.569 0.456
57.8 100.5 0.404 -0.024 0.477 0.073 0.479 -0.027 0.506 0.452
58.6 100.8 0.403 -0.015 0.474 0.018 0.474 -0.015 0.490 0.459
39.4 71.7 0.408 0.029 -0.020 0.018 0.030 -0.022 0.052 0.009
62.2 74.4 0.361 0.084 -0.048 0.052 0.089 -0.053 0.142 0.036
69.7 77.9 0.351 0.170 -0.086 0.068 0.174 -0.090 0.264 0.084
40.3 82.3 0.418 0.020 0.291 0.601 0.485 -0.174 0.659 0.311
46.1 88.2 0.413 -0.167 0.656 0.097 0.659 -0.170 0.829 0.489
48.6 89.0 0.409 -0.125 0.612 0.083 0.615 -0.128 0.742 0.487
52.1 90.3 0.404 -0.061 0.567 0.028 0.567 -0.062 0.629 0.506
53.4 90.6 0.402 -0.034 0.540 0.004 0.540 -0.034 0.574 0.505
123.0 109.7 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000 STRESSES AND STRESS LEVELS FOR FINAL CONDITION AT END OF INCREMENT ELE SIG-X SIG-Y TAU-XY SIG- SIG- TAU-MAX THETA SIG1/SIG3 TAUXY/SIGY SLCRIT SLPRES ELE 0.316 0.616 0.007 0.616 0.316 0.150 1.381 1.951 0.012 0.286 0.278
0.339 0.622 0.034 0.626 0.335 0.146 6.691 1.869 0.054 0.282 0.260
0.413 0.657 0.098 0.691 0.379 0.156 19.363 1.823 0.149 0.273 0.258
0.531 0.918 0.121 0.952 0.497 0.228 15.973 1.917 0.131 0.315 0.315
0.621 1.155 0.069 1.164 0.612 0.276 7.276 1.901 0.060 0.329 0.329
0.683 1.210 0.029 1.212 0.682 0.265 3.195 1.778 0.024 0.292 0.292
0.689 1.202 0.015 1.202 0.689 0.257 1.676 1.745 0.012 0.281 0.281
0.699 1.210 0.004 1.210 0.699 0.255 0.422 1.731 0.003 0.276 0.276
0.101 0.175 0.003 0.175 0.101 0.037 2.006 1.734 0.015 0.135 0.113
0.148 0.175 0.012 0.179 0.143 0.018 20.674 1.253 0.069 0.124 0.049
0.226 0.182 0.017 0.232 0.176 0.028 70.924 1.321 0.096 0.118 0.070
0.320 0.485 0.085 0.521 0.284 0.119 23.037 1.837 0.176 0.233 0.233
0.411 0.767 0.016 0.768 0.410 0.179 2.530 1.872 0.021 0.281 0.281
0.422 0.764 0.014 0.764 0.421 0.172 2.406 1.815 0.019 0.265 0.265
0.459 0.780 0.005 0.780 0.459 0.160 0.938 1.700 0.007 0.235 0.235
0.468 0.774 0.001 0.774 0.468 0.153 0.157 1.653 0.001 0.221 0.221
0.075 0.150 0.034 0.163 0.062 0.050 20.905 2.618 0.224 0.051 0.051
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068 EXAM ********************************************************
********************************************************
* *
* LAYER NUMBER***************************** *
* *
********************************************************
******************************************************** ADDED ELEMENTS******************** THRU
ADDED NODAL POINTS**************** THRU
NODAL POINTS OF HUMPED SURFACE**** BAND WIDTH************************
TOTAL NUMBER OF EQUATIONS*********
NUMBER OF EQUATIONS IN BLOCK******
NUMBER OF BLOCKS****************** NODAL POINT FORCES (WEIGHTS OF ADDED ELEMENTS) NP X-FORCE Y-FORCE 0.000 -2.000
0.000 -5.000
0.000 -6.000
0.000 -6.000
0.000 -3.000
0.000 -5.000
0.000 -6.000
0.000 -6.000
0.000 -3.000 LAYER NUMBER = ITERATION =
*********************************************************** NP DELTA-X DELTA-Y X-DISP Y-DISP TOTAL NP 0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0007 0.0000 0.0018 0.0018
-0.0072 0.0002 -0.0198 0.0007 0.0198
-0.0197 0.0021 -0.0541 0.0060 0.0544
-0.0451 0.0101 -0.1172 0.0125 0.1179
-0.0758 -0.0154 -0.1536 -0.0917 0.1789
-0.0633 -0.0562 -0.0977 -0.1355 0.1671
-0.0326 -0.0676 -0.0483 -0.1390 0.1471
-0.0099 -0.0643 -0.0160 -0.1359 0.1368
0.0000 -0.0605 0.0000 -0.1312 0.1312
0.0000 0.0015 0.0000 0.0042 0.0042
-0.0085 0.0011 -0.0247 0.0041 0.0251
-0.0274 0.0075 -0.0724 0.0184 0.0747
-0.0685 0.0265 -0.1435 0.0390 0.1487
-0.0767 -0.0245 -0.1540 -0.1691 0.2287
-0.0741 -0.1026 -0.1280 -0.2448 0.2763
-0.0390 -0.1256 -0.0615 -0.2565 0.2638
-0.0174 -0.1125 -0.0250 -0.2379 0.2392
0.0000 -0.1079 0.0000 -0.2327 0.2327
-0.0497 -0.0242 -0.0497 -0.0242 0.0553
-0.0418 -0.1290 -0.0418 -0.1290 0.1356
-0.0440 -0.1557 -0.0440 -0.1557 0.1618
-0.0235 -0.1445 -0.0235 -0.1445 0.1464
0.0000 -0.1384 0.0000 -0.1384 0.1384
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000 MODULUS AND POISSON'S RATIO VALUES BASED ON AVERAGE STRESSES DURING THE INCREMENT
STRAINS FOR FINAL CONDITION AT END OF INCREMENT ELE ELAS MOD BULK MOD POIS EPS-X EPS-Y GAM-XY EPS- EPS- GAMMAX EPS-V ELE 54.8 91.6 0.400 0.020 -0.008 0.067 0.042 -0.031 0.073 0.011
68.2 92.9 0.378 0.057 -0.022 0.237 0.143 -0.108 0.250 0.035
53.9 94.8 0.405 0.158 -0.062 0.555 0.347 -0.250 0.597 0.096
52.9 101.2 0.413 0.091 0.264 1.163 0.766 -0.411 1.176 0.355
58.5 106.8 0.409 -0.140 0.757 0.947 0.961 -0.344 1.305 0.618
67.8 110.5 0.398 -0.124 0.915 0.495 0.971 -0.180 1.151 0.791
72.0 111.6 0.393 -0.081 0.916 0.206 0.927 -0.091 1.018 0.836
74.7 112.2 0.389 -0.040 0.890 0.041 0.891 -0.040 0.931 0.850
57.6 73.4 0.369 0.044 -0.029 0.026 0.047 -0.031 0.078 0.015
73.0 79.3 0.347 0.137 -0.079 0.083 0.144 -0.087 0.232 0.057
40.5 80.5 0.416 0.336 -0.195 0.156 0.347 -0.206 0.553 0.141
47.7 91.2 0.413 0.117 0.255 0.914 0.648 -0.276 0.924 0.372
55.7 100.4 0.407 -0.205 0.934 0.452 0.977 -0.248 1.225 0.729
56.2 102.1 0.408 -0.290 1.134 0.255 1.146 -0.301 1.447 0.844
64.1 104.8 0.398 -0.172 1.098 0.057 1.098 -0.173 1.271 0.926
67.3 105.3 0.393 -0.102 1.018 0.020 1.018 -0.103 1.120 0.915
278.2 248.1 0.313 0.041 -0.002 -0.015 0.042 -0.004 0.046 0.039
173.9 155.0 0.313 -0.026 0.131 0.161 0.165 -0.060 0.225 0.105
170.2 151.7 0.313 -0.082 0.283 -0.012 0.283 -0.082 0.366 0.201
160.8 143.4 0.313 -0.105 0.311 -0.005 0.311 -0.105 0.416 0.205
162.1 144.6 0.313 -0.102 0.312 0.004 0.312 -0.102 0.414 0.210
123.0 109.7 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000 STRESSES AND STRESS LEVELS FOR FINAL CONDITION AT END OF INCREMENT ELE SIG-X SIG-Y TAU-XY SIG- SIG- TAU-MAX THETA SIG1/SIG3 TAUXY/SIGY SLCRIT SLPRES ELE 0.322 0.619 0.012 0.619 0.322 0.149 2.322 1.923 0.019 0.285 0.272
0.360 0.629 0.055 0.640 0.349 0.146 11.132 1.835 0.088 0.279 0.254
0.456 0.660 0.135 0.727 0.389 0.169 26.506 1.870 0.205 0.276 0.276
0.644 1.008 0.208 1.102 0.550 0.276 24.377 2.006 0.206 0.357 0.357
0.801 1.447 0.187 1.497 0.751 0.373 15.011 1.993 0.129 0.382 0.382
0.963 1.727 0.114 1.744 0.946 0.399 8.307 1.843 0.066 0.340 0.340
1.021 1.790 0.050 1.794 1.018 0.388 3.671 1.762 0.028 0.312 0.312
1.054 1.802 0.010 1.802 1.054 0.374 0.772 1.710 0.006 0.292 0.292
0.112 0.175 0.004 0.175 0.111 0.032 3.736 1.575 0.024 0.132 0.095
0.189 0.170 0.020 0.202 0.157 0.022 57.141 1.285 0.120 0.121 0.058
0.314 0.191 0.030 0.321 0.184 0.068 76.995 1.742 0.157 0.167 0.167
0.401 0.521 0.138 0.611 0.310 0.151 33.319 1.971 0.266 0.281 0.281
0.605 1.086 0.086 1.101 0.590 0.255 9.855 1.865 0.079 0.313 0.313
0.673 1.289 0.049 1.293 0.670 0.312 4.492 1.931 0.038 0.348 0.348
0.784 1.399 0.012 1.399 0.784 0.308 1.096 1.785 0.008 0.305 0.305
0.801 1.371 0.005 1.371 0.801 0.285 0.472 1.711 0.003 0.278 0.278
0.230 0.213 0.018 0.241 0.202 0.019 57.432 1.193 0.083 0.038 0.017
0.232 0.590 0.107 0.619 0.202 0.208 15.386 3.059 0.181 0.179 0.179
0.261 0.885 -0.008 0.885 0.261 0.312 -0.723 3.388 -0.009 0.253 0.253
0.231 0.891 -0.003 0.891 0.231 0.330 -0.276 3.853 -0.004 0.275 0.275
0.241 0.903 0.002 0.903 0.241 0.331 0.198 3.742 0.003 0.274 0.274
0.075 0.150 0.034 0.163 0.062 0.050 20.905 2.618 0.224 0.051 0.051
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068 EXAM ********************************************************
********************************************************
* *
* LAYER NUMBER***************************** *
* *
********************************************************
******************************************************** ADDED ELEMENTS******************** THRU
ADDED NODAL POINTS**************** THRU
NODAL POINTS OF HUMPED SURFACE**** BAND WIDTH************************
TOTAL NUMBER OF EQUATIONS*********
NUMBER OF EQUATIONS IN BLOCK******
NUMBER OF BLOCKS****************** NODAL POINT FORCES (WEIGHTS OF ADDED ELEMENTS) NP X-FORCE Y-FORCE 0.000 -2.000
0.000 -5.000
0.000 -6.000
0.000 -3.000
0.000 -5.000
0.000 -6.000
0.000 -3.000 LAYER NUMBER = ITERATION =
*********************************************************** NP DELTA-X DELTA-Y X-DISP Y-DISP TOTAL NP 0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0002 0.0000 0.0021 0.0021
-0.0044 0.0003 -0.0241 0.0010 0.0242
-0.0130 0.0009 -0.0670 0.0069 0.0674
-0.0258 0.0052 -0.1431 0.0177 0.1441
-0.0518 0.0028 -0.2054 -0.0889 0.2239
-0.0629 -0.0195 -0.1606 -0.1551 0.2233
-0.0517 -0.0454 -0.1000 -0.1844 0.2097
-0.0267 -0.0594 -0.0427 -0.1953 0.1999
0.0000 -0.0627 0.0000 -0.1939 0.1939
0.0000 0.0008 0.0000 0.0050 0.0050
-0.0053 0.0007 -0.0300 0.0049 0.0304
-0.0172 0.0048 -0.0896 0.0233 0.0926
-0.0480 0.0143 -0.1915 0.0533 0.1988
-0.0587 0.0085 -0.2127 -0.1606 0.2665
-0.0746 -0.0300 -0.2026 -0.2749 0.3415
-0.0629 -0.0850 -0.1244 -0.3415 0.3634
-0.0312 -0.1089 -0.0562 -0.3468 0.3514
0.0000 -0.1144 0.0000 -0.3472 0.3472
-0.0539 0.0117 -0.1036 -0.0126 0.1043
-0.0519 -0.0350 -0.0937 -0.1640 0.1889
-0.0469 -0.1133 -0.0910 -0.2691 0.2840
-0.0230 -0.1500 -0.0465 -0.2944 0.2981
0.0000 -0.1525 0.0000 -0.2909 0.2909
-0.0249 -0.0376 -0.0249 -0.0376 0.0451
-0.0168 -0.1383 -0.0168 -0.1383 0.1394
-0.0156 -0.1773 -0.0156 -0.1773 0.1780
0.0000 -0.1844 0.0000 -0.1844 0.1844
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000 MODULUS AND POISSON'S RATIO VALUES BASED ON AVERAGE STRESSES DURING THE INCREMENT
STRAINS FOR FINAL CONDITION AT END OF INCREMENT ELE ELAS MOD BULK MOD POIS EPS-X EPS-Y GAM-XY EPS- EPS- GAMMAX EPS-V ELE 58.2 91.8 0.394 0.024 -0.010 0.082 0.051 -0.037 0.089 0.014
71.3 93.5 0.373 0.071 -0.026 0.294 0.177 -0.132 0.310 0.045
49.3 95.2 0.414 0.190 -0.082 0.673 0.417 -0.309 0.726 0.108
50.6 102.3 0.418 0.156 0.238 1.428 0.912 -0.518 1.430 0.394
56.3 109.3 0.414 -0.112 0.813 1.386 1.184 -0.482 1.666 0.701
69.9 115.5 0.399 -0.152 1.131 0.942 1.286 -0.306 1.592 0.980
77.8 118.1 0.390 -0.143 1.266 0.503 1.309 -0.187 1.496 1.122
83.0 119.5 0.384 -0.107 1.297 0.139 1.301 -0.110 1.411 1.191
62.7 74.6 0.360 0.054 -0.034 0.031 0.057 -0.037 0.094 0.020
73.2 79.4 0.346 0.171 -0.101 0.102 0.180 -0.110 0.290 0.070
39.8 82.5 0.420 0.445 -0.260 0.253 0.467 -0.282 0.749 0.185
42.9 90.9 0.421 0.209 0.180 1.080 0.735 -0.346 1.080 0.389
66.4 105.1 0.395 -0.137 0.957 0.697 1.059 -0.239 1.298 0.820
59.5 108.5 0.409 -0.347 1.385 0.572 1.431 -0.393 1.824 1.037
68.0 112.6 0.399 -0.314 1.543 0.230 1.550 -0.321 1.871 1.230
72.2 113.6 0.394 -0.247 1.524 0.065 1.525 -0.248 1.772 1.277
203.8 181.7 0.313 0.094 -0.033 -0.034 0.097 -0.036 0.132 0.061
177.3 158.1 0.313 0.009 0.140 0.236 0.209 -0.061 0.270 0.149
158.5 141.3 0.313 -0.124 0.449 0.127 0.456 -0.131 0.587 0.326
125.9 112.2 0.313 -0.245 0.658 0.026 0.658 -0.245 0.902 0.413
133.2 118.8 0.313 -0.238 0.708 -0.017 0.708 -0.238 0.945 0.470
130.2 116.1 0.313 -0.010 0.027 -0.036 0.034 -0.018 0.052 0.017
172.4 153.7 0.313 -0.033 0.139 0.162 0.171 -0.065 0.236 0.106
181.1 161.5 0.313 -0.063 0.262 0.001 0.262 -0.063 0.325 0.199
167.1 148.9 0.313 -0.097 0.297 -0.013 0.297 -0.097 0.393 0.200
123.0 109.7 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000
139.3 124.2 0.313 0.000 0.000 0.000 0.000 0.000 0.000 0.000 STRESSES AND STRESS LEVELS FOR FINAL CONDITION AT END OF INCREMENT ELE SIG-X SIG-Y TAU-XY SIG- SIG- TAU-MAX THETA SIG1/SIG3 TAUXY/SIGY SLCRIT SLPRES ELE 0.326 0.620 0.015 0.621 0.325 0.148 2.929 1.907 0.024 0.284 0.268
0.375 0.635 0.070 0.652 0.357 0.148 14.135 1.826 0.110 0.277 0.253
0.477 0.663 0.156 0.751 0.389 0.181 29.633 1.933 0.235 0.295 0.295
0.702 1.034 0.255 1.172 0.563 0.304 28.475 2.080 0.247 0.386 0.386
0.893 1.550 0.274 1.649 0.794 0.428 19.911 2.078 0.177 0.420 0.420
1.135 2.021 0.225 2.075 1.081 0.497 13.484 1.920 0.112 0.381 0.381
1.272 2.271 0.132 2.288 1.254 0.517 7.423 1.824 0.058 0.349 0.349
1.353 2.385 0.039 2.386 1.351 0.517 2.172 1.766 0.016 0.328 0.328
0.119 0.175 0.005 0.176 0.118 0.029 5.255 1.487 0.030 0.130 0.084
0.215 0.166 0.025 0.226 0.155 0.035 66.979 1.453 0.153 0.121 0.092
0.377 0.205 0.044 0.387 0.195 0.096 76.518 1.991 0.213 0.230 0.230
0.443 0.512 0.163 0.644 0.310 0.167 39.009 2.075 0.319 0.312 0.312
0.719 1.179 0.145 1.221 0.677 0.272 16.071 1.802 0.123 0.303 0.301
0.831 1.577 0.116 1.595 0.814 0.390 8.608 1.960 0.073 0.376 0.376
1.008 1.908 0.054 1.911 1.005 0.453 3.419 1.902 0.028 0.369 0.369
1.074 1.981 0.016 1.982 1.074 0.454 1.026 1.845 0.008 0.349 0.349
0.342 0.194 0.003 0.342 0.194 0.074 88.994 1.762 0.013 0.064 0.064
0.328 0.652 0.157 0.716 0.264 0.226 22.109 2.706 0.241 0.182 0.182
0.337 1.212 0.076 1.218 0.331 0.444 4.950 3.685 0.063 0.337 0.337
0.265 1.390 0.012 1.390 0.265 0.563 0.589 5.252 0.008 0.455 0.455
0.324 1.524 -0.008 1.524 0.324 0.600 -0.395 4.701 -0.005 0.459 0.459
0.079 0.190 0.015 0.193 0.077 0.058 7.759 2.504 0.081 0.057 0.057
0.223 0.598 0.106 0.626 0.195 0.215 14.791 3.206 0.178 0.187 0.187
0.293 0.891 0.001 0.891 0.293 0.299 0.063 3.037 0.001 0.235 0.235
0.240 0.890 -0.008 0.890 0.240 0.325 -0.738 3.708 -0.009 0.269 0.269
0.075 0.150 0.034 0.163 0.062 0.050 20.905 2.618 0.224 0.051 0.051
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068
0.150 0.300 0.000 0.300 0.150 0.075 0.000 2.000 0.000 0.068 0.068 EXAM ********************************************************
********************************************************
* *
* LOAD CASE AFTER CONSTRUCTION************* *
* *
********************************************************
******************************************************** BAND WIDTH************************
TOTAL NUMBER OF EQUATIONS*********
NUMBER OF EQUATIONS IN BLOCK******
NUMBER OF BLOCKS****************** NUMBER OF N.P. FORCE CARDS********
NUMBER OF PRESSURE CARDS**********
PRESSURE BOUNDARY CONDITIONS I J PRESSURE I PRESSURE J 0.100 0.200
0.200 0.100 NODAL POINT FORCES NP X-FORCE Y-FORCE 0.000 -3.000
0.000 -6.000
0.000 -4.000
0.000 -3.000
0.000 -2.000
0.000 -1.000
0.000 -1.333
0.000 -3.333
0.000 -1.333 LOAD CASE = ITERATION =
*********************************************************** NP DELTA-X DELTA-Y X-DISP Y-DISP TOTAL NP 0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 0.0000 0.0000 0.0000 0.0000
0.0000 -0.0109 0.0000 -0.0089 0.0089
-0.0031 -0.0204 -0.0273 -0.0195 0.0335
-0.0010 -0.0206 -0.0680 -0.0136 0.0694
0.0012 -0.0181 -0.1419 -0.0004 0.1419
0.0010 -0.0095 -0.2045 -0.0985 0.2269
-0.0040 -0.0056 -0.1646 -0.1606 0.2300
-0.0076 -0.0081 -0.1076 -0.1925 0.2205
-0.0056 -0.0123 -0.0482 -0.2076 0.2131
0.0000 -0.0137 0.0000 -0.2076 0.2076
0.0000 -0.0198 0.0000 -0.0148 0.0148
-0.0010 -0.0350 -0.0310 -0.0302 0.0433
-0.0021 -0.0318 -0.0917 -0.0085 0.0921
-0.0057 -0.0320 -0.1972 0.0213 0.1984
-0.0048 -0.0155 -0.2175 -0.1761 0.2799
-0.0090 -0.0079 -0.2116 -0.2828 0.3532
-0.0112 -0.0140 -0.1356 -0.3555 0.3805
-0.0078 -0.0225 -0.0640 -0.3693 0.3748
0.0000 -0.0256 0.0000 -0.3727 0.3727
-0.0132 -0.0183 -0.1168 -0.0309 0.1208
-0.0098 -0.0098 -0.1034 -0.1738 0.2023
-0.0101 -0.0185 -0.1011 -0.2875 0.3048
-0.0068 -0.0321 -0.0533 -0.3266 0.3309
0.0000 -0.0355 0.0000 -0.3264 0.3264
-0.0103 -0.0128 -0.0352 -0.0505 0.0615
-0.0065 -0.0220 -0.0233 -0.1604 0.1620
-0.0034 -0.0399 -0.0190 -0.2172 0.2181
0.0000 -0.0437 0.0000 -0.2281 0.2281
0.0003 -0.0250 0.0003 -0.0250 0.0250
0.0018 -0.0482 0.0018 -0.0482 0.0482
0.0000 -0.0477 0.0000 -0.0477 0.0477 MODULUS AND POISSON'S RATIO VALUES BASED ON AVERAGE STRESSES DURING THE INCREMENT
STRAINS FOR FINAL CONDITION AT END OF INCREMENT ELE ELAS MOD BULK MOD POIS EPS-X EPS-Y GAM-XY EPS- EPS- GAMMAX EPS-V ELE 57.0 94.3 0.399 0.027 0.094 0.101 0.122 0.000 0.122 0.122
60.4 96.2 0.395 0.068 0.110 0.308 0.245 -0.066 0.311 0.178
56.7 97.8 0.403 0.185 0.047 0.667 0.456 -0.225 0.681 0.232
66.4 104.4 0.394 0.156 0.330 1.400 0.948 -0.462 1.410 0.486
66.6 110.9 0.400 -0.100 0.864 1.386 1.226 -0.462 1.688 0.764
72.2 117.5 0.398 -0.143 1.177 0.987 1.341 -0.307 1.648 1.035
79.6 121.0 0.390 -0.148 1.334 0.557 1.384 -0.199 1.583 1.185
85.7 122.8 0.384 -0.121 1.384 0.161 1.388 -0.125 1.513 1.263
53.9 79.5 0.387 0.058 0.083 0.045 0.096 0.045 0.051 0.142
88.8 88.9 0.333 0.169 0.028 0.091 0.183 0.014 0.168 0.197
78.6 88.4 0.352 0.449 -0.134 0.288 0.482 -0.168 0.650 0.315
59.0 94.0 0.395 0.207 0.280 1.081 0.785 -0.298 1.083 0.487
73.2 107.6 0.387 -0.114 0.999 0.722 1.106 -0.221 1.327 0.885
65.5 111.2 0.402 -0.333 1.426 0.636 1.482 -0.388 1.870 1.093
69.0 115.8 0.401 -0.327 1.624 0.291 1.634 -0.338 1.973 1.296
73.2 117.4 0.396 -0.280 1.635 0.087 1.636 -0.281 1.917 1.354
354.2 315.8 0.313 0.090 -0.006 -0.033 0.092 -0.009 0.101 0.084
188.7 168.3 0.313 0.011 0.163 0.242 0.230 -0.056 0.286 0.174
159.2 141.9 0.313 -0.117 0.481 0.163 0.492 -0.128 0.620 0.364
113.1 108.5 0.326 -0.261 0.728 0.071 0.730 -0.263 0.992 0.467
118.4 119.0 0.334 -0.274 0.806 -0.006 0.806 -0.274 1.080 0.532
129.6 115.6 0.313 -0.027 0.057 -0.073 0.071 -0.041 0.112 0.030
160.5 143.1 0.313 -0.041 0.171 0.191 0.208 -0.078 0.286 0.130
174.6 155.7 0.313 -0.079 0.319 0.045 0.320 -0.080 0.400 0.240
151.2 134.8 0.313 -0.122 0.376 -0.013 0.376 -0.122 0.499 0.254
124.8 111.3 0.313 -0.019 0.030 -0.022 0.033 -0.021 0.054 0.011
177.8 158.5 0.313 -0.012 0.056 0.043 0.063 -0.018 0.081 0.045
184.7 164.7 0.313 -0.004 0.061 -0.018 0.063 -0.005 0.068 0.057 STRESSES AND STRESS LEVELS FOR FINAL CONDITION AT END OF INCREMENT ELE SIG-X SIG-Y TAU-XY SIG- SIG- TAU-MAX THETA SIG1/SIG3 TAUXY/SIGY SLCRIT SLPRES ELE 0.414 0.749 0.019 0.750 0.413 0.169 3.254 1.816 0.025 0.267 0.264
0.482 0.803 0.073 0.818 0.466 0.176 12.228 1.755 0.091 0.259 0.255
0.579 0.819 0.154 0.894 0.504 0.195 26.105 1.776 0.189 0.277 0.268
0.784 1.159 0.248 1.283 0.660 0.311 26.451 1.943 0.214 0.371 0.351
0.958 1.634 0.274 1.731 0.861 0.435 19.532 2.010 0.168 0.411 0.400
1.195 2.100 0.237 2.158 1.136 0.511 13.828 1.899 0.113 0.376 0.375
1.333 2.374 0.148 2.395 1.312 0.541 7.935 1.825 0.062 0.352 0.352
1.418 2.512 0.046 2.514 1.417 0.549 2.406 1.775 0.018 0.334 0.334
0.201 0.302 0.008 0.303 0.201 0.051 4.513 1.508 0.026 0.120 0.120
0.299 0.337 0.022 0.347 0.289 0.029 24.436 1.202 0.065 0.104 0.057
0.468 0.368 0.054 0.492 0.344 0.074 66.577 1.428 0.146 0.199 0.129
0.520 0.632 0.163 0.749 0.404 0.173 35.518 1.856 0.258 0.292 0.275
0.790 1.260 0.151 1.304 0.745 0.279 16.370 1.750 0.120 0.296 0.288
0.891 1.650 0.131 1.672 0.870 0.401 9.503 1.922 0.079 0.370 0.366
1.067 2.014 0.069 2.019 1.062 0.478 4.138 1.900 0.034 0.371 0.371
1.134 2.116 0.022 2.117 1.133 0.492 1.288 1.868 0.010 0.362 0.362
0.381 0.321 0.005 0.382 0.320 0.031 85.235 1.193 0.016 0.057 0.024
0.361 0.715 0.161 0.778 0.299 0.240 21.183 2.604 0.226 0.187 0.187
0.384 1.289 0.098 1.300 0.374 0.463 6.088 3.479 0.076 0.339 0.339
0.294 1.494 0.031 1.494 0.293 0.601 1.475 5.104 0.021 0.473 0.473
0.347 1.667 -0.003 1.667 0.347 0.660 -0.140 4.802 -0.002 0.494 0.494
0.073 0.231 -0.003 0.231 0.073 0.079 -0.991 3.182 -0.012 0.079 0.079
0.238 0.663 0.124 0.697 0.204 0.246 15.153 3.412 0.187 0.211 0.211
0.317 1.012 0.030 1.013 0.316 0.349 2.446 3.208 0.029 0.268 0.268
0.263 1.035 -0.008 1.035 0.263 0.386 -0.596 3.930 -0.008 0.312 0.312
0.066 0.188 0.023 0.192 0.062 0.065 10.402 3.107 0.123 0.065 0.065
0.185 0.427 0.029 0.431 0.181 0.125 6.754 2.374 0.068 0.110 0.110
0.212 0.454 -0.012 0.455 0.211 0.122 -2.919 2.150 -0.027 0.104 0.104
feadam84计算结果原始数据.dat
为了节省时间首先按 datapacking=point格式把节点的处理了，因为这种格式节点的变量可以直接跟在节点后面：
title = "feadam 2d model post-process"
variables = "x"
"y"
"delta-x"
"delta-y"
"x-disp"
"y-disp"
"total" zone t="LOAD CASE AFTER CONSTRUCTION 1"
strandid=, solutiontime=
nodes=, elements=, zonetype=fequadrilateral
datapacking=point
0.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
50.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
80.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
100.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
120.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
140.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
160.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
180.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
200.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000
0.000 15.000 0.0000 -0.0109 0.0000 -0.0089 0.0089
50.000 15.000 -0.0031 -0.0204 -0.0273 -0.0195 0.0335
80.000 15.000 -0.0010 -0.0206 -0.0680 -0.0136 0.0694
100.000 15.000 0.0012 -0.0181 -0.1419 -0.0004 0.1419
120.000 15.000 0.0010 -0.0095 -0.2045 -0.0985 0.2269
140.000 15.000 -0.0040 -0.0056 -0.1646 -0.1606 0.2300
160.000 15.000 -0.0076 -0.0081 -0.1076 -0.1925 0.2205
180.000 15.000 -0.0056 -0.0123 -0.0482 -0.2076 0.2131
200.000 15.000 0.0000 -0.0137 0.0000 -0.2076 0.2076
0.000 25.000 0.0000 -0.0198 0.0000 -0.0148 0.0148
50.000 25.000 -0.0010 -0.0350 -0.0310 -0.0302 0.0433
80.000 25.000 -0.0021 -0.0318 -0.0917 -0.0085 0.0921
100.000 25.000 -0.0057 -0.0320 -0.1972 0.0213 0.1984
120.000 25.000 -0.0048 -0.0155 -0.2175 -0.1761 0.2799
140.000 25.000 -0.0090 -0.0079 -0.2116 -0.2828 0.3532
160.000 25.000 -0.0112 -0.0140 -0.1356 -0.3555 0.3805
180.000 25.000 -0.0078 -0.0225 -0.0640 -0.3693 0.3748
200.000 25.000 0.0000 -0.0256 0.0000 -0.3727 0.3727
120.000 35.000 -0.0132 -0.0183 -0.1168 -0.0309 0.1208
140.000 35.000 -0.0098 -0.0098 -0.1034 -0.1738 0.2023
160.000 35.000 -0.0101 -0.0185 -0.1011 -0.2875 0.3048
180.000 35.000 -0.0068 -0.0321 -0.0533 -0.3266 0.3309
200.000 35.000 0.0000 -0.0355 0.0000 -0.3264 0.3264
140.000 45.000 -0.0103 -0.0128 -0.0352 -0.0505 0.0615
160.000 45.000 -0.0065 -0.0220 -0.0233 -0.1604 0.1620
180.000 45.000 -0.0034 -0.0399 -0.0190 -0.2172 0.2181
200.000 45.000 0.0000 -0.0437 0.0000 -0.2281 0.2281
160.000 55.000 0.0003 -0.0250 0.0003 -0.0250 0.0250
180.000 55.000 0.0018 -0.0482 0.0018 -0.0482 0.0482
200.000 55.000 0.0000 -0.0477 0.0000 -0.0477 0.0477
tecplot加载上面的dat后，输出上述数据为BLOCK格式（因为要显示单元变量只能用block数据格式），方法如下：
点击ok就可以输出block格式的数据了。删除不要的，比如单元之间连接。
很明显下图这儿这样的数据是组成单元的节点编号：
在这些节点编号之前要输入所有数据，且是block即成块的格式，可以用notepad++配合excel的选择性粘贴里转置功能将列转换成行（因为计算结果中好多变量都是按单元号成列给出的，而block格式要求相同的单元变量比如sigx要在一行或临近的一行（块））
结果如下：
TITLE = "feadam 2d model post-process"
VARIABLES = "x"
"y"
"delta-x"
"delta-y"
"x-disp"
"y-disp"
"total"
ELAS-MOD BULK-MOD POIS EPS-X EPS-Y GAM-XY EPS- EPS- GAMMAX EPS-V
SIG-X SIG-Y TAU-XY SIG- SIG- TAU-MAX THETA SIG1/SIG3 TAUXY/SIGY SLCRIT SLPRES ZONE T="LOAD CASE AFTER CONSTRUCTION 1"
STRANDID=, SOLUTIONTIME=
Nodes=, Elements=, ZONETYPE=FEQuadrilateral
DATAPACKING=BLOCK
varlocation=([-]=cellcentered) 0.000000000E+000 5.000000000E+001 8.000000000E+001 1.000000000E+002 1.200000000E+002
1.400000000E+002 1.600000000E+002 1.800000000E+002 2.000000000E+002 0.000000000E+000
5.000000000E+001 8.000000000E+001 1.000000000E+002 1.200000000E+002 1.400000000E+002
1.600000000E+002 1.800000000E+002 2.000000000E+002 0.000000000E+000 5.000000000E+001
8.000000000E+001 1.000000000E+002 1.200000000E+002 1.400000000E+002 1.600000000E+002
1.800000000E+002 2.000000000E+002 1.200000000E+002 1.400000000E+002 1.600000000E+002
1.800000000E+002 2.000000000E+002 1.400000000E+002 1.600000000E+002 1.800000000E+002
2.000000000E+002 1.600000000E+002 1.800000000E+002 2.000000000E+002
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 1.500000000E+001
1.500000000E+001 1.500000000E+001 1.500000000E+001 1.500000000E+001 1.500000000E+001
1.500000000E+001 1.500000000E+001 1.500000000E+001 2.500000000E+001 2.500000000E+001
2.500000000E+001 2.500000000E+001 2.500000000E+001 2.500000000E+001 2.500000000E+001
2.500000000E+001 2.500000000E+001 3.500000000E+001 3.500000000E+001 3.500000000E+001
3.500000000E+001 3.500000000E+001 4.500000000E+001 4.500000000E+001 4.500000000E+001
4.500000000E+001 5.500000000E+001 5.500000000E+001 5.500000000E+001
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
-3.100000089E-003 -1.000000047E-003 1.200000057E-003 1.000000047E-003 -4.000000190E-003
-7.600000128E-003 -5.599999800E-003 0.000000000E+000 0.000000000E+000 -1.000000047E-003
-2.099999925E-003 -5.700000096E-003 -4.800000228E-003 -8.999999613E-003 -1.119999960E-002
-7.799999788E-003 0.000000000E+000 -1.319999993E-002 -9.800000116E-003 -1.009999961E-002
-6.800000090E-003 0.000000000E+000 -1.030000020E-002 -6.500000134E-003 -3.400000045E-003
0.000000000E+000 3.000000142E-004 1.799999969E-003 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 -1.090000011E-002
-2.040000074E-002 -2.060000040E-002 -1.810000092E-002 -9.499999695E-003 -5.599999800E-003
-8.100000210E-003 -1.229999959E-002 -1.370000001E-002 -1.979999989E-002 -3.500000015E-002
-3.180000186E-002 -3.200000152E-002 -1.549999975E-002 -7.899999619E-003 -1.400000043E-002
-2.250000089E-002 -2.559999935E-002 -1.830000058E-002 -9.800000116E-003 -1.850000024E-002
-3.209999949E-002 -3.550000116E-002 -1.279999968E-002 -2.199999988E-002 -3.990000114E-002
-4.369999841E-002 -2.500000037E-002 -4.820000008E-002 -4.769999906E-002
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
-2.730000019E-002 -6.800000370E-002 -1.419000030E-001 -2.045000046E-001 -1.645999998E-001
-1.076000035E-001 -4.820000008E-002 0.000000000E+000 0.000000000E+000 -3.099999949E-002
-9.170000255E-002 -1.972000003E-001 -2.175000012E-001 -2.116000056E-001 -1.356000006E-001
-6.400000304E-002 0.000000000E+000 -1.168000028E-001 -1.033999994E-001 -1.010999978E-001
-5.330000073E-002 0.000000000E+000 -3.519999981E-002 -2.329999954E-002 -1.899999939E-002
0.000000000E+000 3.000000142E-004 1.799999969E-003 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 -8.899999782E-003
-1.950000040E-002 -1.360000018E-002 -3.999999899E-004 -9.849999845E-002 -1.606000066E-001
-1.924999952E-001 -2.075999975E-001 -2.075999975E-001 -1.480000000E-002 -3.020000085E-002
-8.500000462E-003 2.129999921E-002 -1.761000007E-001 -2.827999890E-001 -3.555000126E-001
-3.693000078E-001 -3.727000058E-001 -3.089999966E-002 -1.738000065E-001 -2.874999940E-001
-3.265999854E-001 -3.264000118E-001 -5.050000176E-002 -1.604000032E-001 -2.171999961E-001
-2.281000018E-001 -2.500000037E-002 -4.820000008E-002 -4.769999906E-002
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000
0.000000000E+000 0.000000000E+000 0.000000000E+000 0.000000000E+000 8.899999782E-003
3.350000083E-002 6.939999759E-002 1.419000030E-001 2.268999964E-001 2.300000042E-001
2.205000073E-001 2.131000012E-001 2.075999975E-001 1.480000000E-002 4.329999909E-002
9.210000187E-002 1.984000057E-001 2.799000144E-001 3.531999886E-001 3.804999888E-001
3.747999966E-001 3.727000058E-001 1.208000034E-001 2.022999972E-001 3.048000038E-001
3.309000134E-001 3.264000118E-001 6.150000170E-002 1.620000005E-001 2.180999964E-001
2.281000018E-001 2.500000037E-002 4.820000008E-002 4.769999906E-002 60.4 56.7 66.4 66.6 72.2 79.6 85.7 53.9 88.8 78.6 73.2 65.5 73.2 354.2 188.7 159.2 113.1 118.4 129.6 160.5 174.6 151.2 124.8 177.8 184.7
94.3 96.2 97.8 104.4 110.9 117.5 122.8 79.5 88.9 88.4 107.6 111.2 115.8 117.4 315.8 168.3 141.9 108.5 115.6 143.1 155.7 134.8 111.3 158.5 164.7
0.399 0.395 0.403 0.394 0.4 0.398 0.39 0.384 0.387 0.333 0.352 0.395 0.387 0.402 0.401 0.396 0.313 0.313 0.313 0.326 0.334 0.313 0.313 0.313 0.313 0.313 0.313 0.313
0.027 0.068 0.185 0.156 -0.1 -0.143 -0.148 -0.121 0.058 0.169 0.449 0.207 -0.114 -0.333 -0.327 -0.28 0.09 0.011 -0.117 -0.261 -0.274 -0.027 -0.041 -0.079 -0.122 -0.019 -0.012 -0.004
0.094 0.11 0.047 0.33 0.864 1.177 1.334 1.384 0.083 0.028 -0.134 0.28 0.999 1.426 1.624 1.635 -0.006 0.163 0.481 0.728 0.806 0.057 0.171 0.319 0.376 0.03 0.056 0.061
0.101 0.308 0.667 1.4 1.386 0.987 0.557 0.161 0.045 0.091 0.288 1.081 0.722 0.636 0.291 0.087 -0.033 0.242 0.163 0.071 -0.006 -0.073 0.191 0.045 -0.013 -0.022 0.043 -0.018
0.122 0.245 0.456 0.948 1.226 1.341 1.384 1.388 0.096 0.183 0.482 0.785 1.106 1.482 1.634 1.636 0.092 0.23 0.492 0.73 0.806 0.071 0.208 0.32 0.376 0.033 0.063 0.063
-0.066 -0.225 -0.462 -0.462 -0.307 -0.199 -0.125 0.045 0.014 -0.168 -0.298 -0.221 -0.388 -0.338 -0.281 -0.009 -0.056 -0.128 -0.263 -0.274 -0.041 -0.078 -0.08 -0.122 -0.021 -0.018 -0.005
0.122 0.311 0.681 1.41 1.688 1.648 1.583 1.513 0.051 0.168 0.65 1.083 1.327 1.87 1.973 1.917 0.101 0.286 0.62 0.992 1.08 0.112 0.286 0.4 0.499 0.054 0.081 0.068
0.122 0.178 0.232 0.486 0.764 1.035 1.185 1.263 0.142 0.197 0.315 0.487 0.885 1.093 1.296 1.354 0.084 0.174 0.364 0.467 0.532 0.03 0.13 0.24 0.254 0.011 0.045 0.057 0.414 0.482 0.579 0.784 0.958 1.195 1.333 1.418 0.201 0.299 0.468 0.52 0.79 0.891 1.067 1.134 0.381 0.361 0.384 0.294 0.347 0.073 0.238 0.317 0.263 0.066 0.185 0.212
0.749 0.803 0.819 1.159 1.634 2.1 2.374 2.512 0.302 0.337 0.368 0.632 1.26 1.65 2.014 2.116 0.321 0.715 1.289 1.494 1.667 0.231 0.663 1.012 1.035 0.188 0.427 0.454
0.019 0.073 0.154 0.248 0.274 0.237 0.148 0.046 0.008 0.022 0.054 0.163 0.151 0.131 0.069 0.022 0.005 0.161 0.098 0.031 -0.003 -0.003 0.124 0.03 -0.008 0.023 0.029 -0.012
0.75 0.818 0.894 1.283 1.731 2.158 2.395 2.514 0.303 0.347 0.492 0.749 1.304 1.672 2.019 2.117 0.382 0.778 1.3 1.494 1.667 0.231 0.697 1.013 1.035 0.192 0.431 0.455
0.413 0.466 0.504 0.66 0.861 1.136 1.312 1.417 0.201 0.289 0.344 0.404 0.745 0.87 1.062 1.133 0.32 0.299 0.374 0.293 0.347 0.073 0.204 0.316 0.263 0.062 0.181 0.211
0.169 0.176 0.195 0.311 0.435 0.511 0.541 0.549 0.051 0.029 0.074 0.173 0.279 0.401 0.478 0.492 0.031 0.24 0.463 0.601 0.66 0.079 0.246 0.349 0.386 0.065 0.125 0.122
3.254 12.228 26.105 26.451 19.532 13.828 7.935 2.406 4.513 24.436 66.577 35.518 16.37 9.503 4.138 1.288 85.235 21.183 6.088 1.475 -0.14 -0.991 15.153 2.446 -0.596 10.402 6.754 -2.919
1.816 1.755 1.776 1.943 2.01 1.899 1.825 1.775 1.508 1.202 1.428 1.856 1.75 1.922 1.9 1.868 1.193 2.604 3.479 5.104 4.802 3.182 3.412 3.208 3.93 3.107 2.374 2.15
0.025 0.091 0.189 0.214 0.168 0.113 0.062 0.018 0.026 0.065 0.146 0.258 0.12 0.079 0.034 0.01 0.016 0.226 0.076 0.021 -0.002 -0.012 0.187 0.029 -0.008 0.123 0.068 -0.027
0.267 0.259 0.277 0.371 0.411 0.376 0.352 0.334 0.12 0.104 0.199 0.292 0.296 0.37 0.371 0.362 0.057 0.187 0.339 0.473 0.494 0.079 0.211 0.268 0.312 0.065 0.11 0.104
0.264 0.255 0.268 0.351 0.4 0.375 0.352 0.334 0.12 0.057 0.129 0.275 0.288 0.366 0.371 0.362 0.024 0.187 0.339 0.473 0.494 0.079 0.211 0.268 0.312 0.065 0.11 0.104
最终出图用的.dat
1-学习tecplot360的更多相关文章
- 从直播编程到直播教育：LiveEdu.tv开启多元化的在线学习直播时代
2015年9月,一个叫Livecoding.tv的网站在互联网上引起了编程界的注意.缘于Pingwest品玩的一位编辑在上网时无意中发现了这个网站,并写了一篇文章<一个比直播睡觉更奇怪的网站:直 ...
- Angular2学习笔记（1）
Angular2学习笔记(1) 1. 写在前面 之前基于Electron写过一个Markdown编辑器.就其功能而言,主要功能已经实现,一些小的不影响使用的功能由于时间关系还没有完成:但就代码而言,之 ...
- ABP入门系列（1）——学习Abp框架之实操演练
作为.Net工地搬砖长工一名,一直致力于挖坑(Bug)填坑(Debug),但技术却不见长进.也曾热情于新技术的学习,憧憬过成为技术大拿.从前端到后端,从bootstrap到javascript,从py ...
- 消息队列——RabbitMQ学习笔记
消息队列--RabbitMQ学习笔记 1. 写在前面 昨天简单学习了一个消息队列项目--RabbitMQ,今天趁热打铁,将学到的东西记录下来. 学习的资料主要是官网给出的6个基本的消息发送/接收模型, ...
- js学习笔记：webpack基础入门（一）
之前听说过webpack,今天想正式的接触一下,先跟着webpack的官方用户指南走: 在这里有: 如何安装webpack 如何使用webpack 如何使用loader 如何使用webpack的开发者 ...
- Unity3d学习 制作地形
这周学习了如何在unity中制作地形,就是在一个Terrain的对象上盖几座小山,在山底种几棵树,那就讲一下如何完成上述内容. 1.在新键得项目的游戏的Hierarchy目录中新键一个Terrain对 ...
- 《Django By Example》第四章 中文 翻译 （个人学习，渣翻）
书籍出处:https://www.packtpub.com/web-development/django-example 原作者:Antonio Melé (译者注:祝大家新年快乐,这次带来<D ...
- 菜鸟Python学习笔记第一天：关于一些函数库的使用
2017年1月3日 星期二 大一学习一门新的计算机语言真的很难,有时候连函数拼写出错查错都能查半天,没办法,谁让我英语太渣. 关于计算机语言的学习我想还是从C语言学习开始为好,Python有很多语言的 ...
- 多线程爬坑之路-学习多线程需要来了解哪些东西?(concurrent并发包的数据结构和线程池,Locks锁，Atomic原子类)
前言:刚学习了一段机器学习,最近需要重构一个java项目,又赶过来看java.大多是线程代码,没办法,那时候总觉得多线程是个很难的部分很少用到,所以一直没下决定去啃,那些年留下的坑,总是得自己跳进去填 ...
- node.js学习（三）简单的node程序&&模块简单使用&&commonJS规范&&深入理解模块原理
一.一个简单的node程序 1.新建一个txt文件 2.修改后缀 修改之后会弹出这个,点击"是" 3.运行test.js 源文件 使用node.js运行之后的. 如果该路径下没有该 ...
随机推荐
- node-gyp和node-pre-gyp笔记
node-gyp大家都不陌生,先不做赘述. node-pre-gyp,install命令可以将存在网络上的作者根据不同平台预编译好的二进制文件下载下来 因为项目需要,博主需要本地编译,而不是去网上下载 ...
- NodeJS client code websocket
var WebSocketClient = require('websocket').client; var client = new WebSocketClient(); client.on('co ...
- 1.微信小程序里如何设置当地时间？
方法一: 1.效果图 2.wxml code: <!--pages/index/index.wxml--> <text>当前时间:{{time}}</text> & ...
- spring 之 类型转换 2
spring内置的转换器 在spring xml 文件中,配置属性的时候, 不管实际是 list 还是map ,还是Date, 或者原生的java 类型, 我们只能配置xml 给它们. 那么 spri ...
- filter in Servlet
Servlet过滤器: Servlet过滤器是用于执行某些过滤任务的对象.过滤器可以应用于servlet,jsp或html. Servlet过滤器主要用于以下任务: 预处理: Servlet过滤器用于 ...
- 为何要使用ViewModel
ViewModel类是用来存储和管理与UI相关的数据,在设计之初就考虑到生命周期的影响.ViewModel允许数据在屏幕旋转等配置变化后存活. Android framework管理UI控制器(如Ac ...
- kubernetes中service yaml文件的port作用
yaml文件 [root@k8s-master ~]# cat service-hello.yaml apiVersion: v1 kind: Service metadata: name: serv ...
- leetcode160
/** * Definition for singly-linked list. * public class ListNode { * public int val; * public ListNo ...
- POI richText和html的转换案例
private XSSFRichTextString parseHtmlStrToRichText(String htmlStr) { Document document = parseHtmlStr ...
- LeetCode OJ 117. Populating Next Right Pointers in Each Node II
题目 Given a binary tree struct TreeLinkNode { TreeLinkNode *left; TreeLinkNode *right; TreeLinkNode * ...