tekla imort from staad-by engr. atul saxena
DESCRIPTION
Tekla Tutorial By Engr. Atul saxenaTRANSCRIPT
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Staad Model Import To Tekla-Submited By
Atul Saxena B.E(Structures),AIV,
AMIE(Civil) Chartered Engineer.
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First open Tekla India environment---> Open new model---> File----> Import----> FEM--->Properties--->STADD---Select material IS2062 or don't change it material we will change it after importing it To Tekla ---> Parameter--->Access input file as std file (which is pasted on desktop-Use same std file which is attached herewith)
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--->Type--> STADD---Apply--OK (Of same Import FEM window) ----Select OK (Import model window)
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Click Import in above window
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Select accept all Click Yes to save the model. Double click in model outside to view ---view properties Adjust depth to view entire model.
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Right click in model----> fit work as shown below
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*Transmission Tower Design With Connetions.Example. (Input File) Copy and paste these commands to your staad input file browser
************************************************************************
STAAD TRUSS
START JOB INFORMATION
ENGINEER DATE 25-Mar-09
END JOB INFORMATION
INPUT WIDTH 79
INPUT WIDTH 79
UNIT METER KN
JOINT COORDINATES
1 3.000 0.000 3.000
2 1.200 27.000 1.200
3 2.800 3.000 2.800
4 2.600 6.000 2.600
5 2.400 9.000 2.400
6 2.200 12.000 2.200
7 2.000 15.000 2.000
8 1.800 18.000 1.800
14
9 1.600 21.000 1.600
10 1.400 24.000 1.400
11 -3.000 0.000 3.000
12 -1.200 27.000 1.200
13 -2.800 3.000 2.800
14 -2.600 6.000 2.600
15 -2.400 9.000 2.400
16 -2.200 12.000 2.200
17 -2.000 15.000 2.000
18 -1.800 18.000 1.800
19 -1.600 21.000 1.600
20 -1.400 24.000 1.400
21 3.000 0.000 -3.000
22 1.200 27.000 -1.200
23 2.800 3.000 -2.800
15
24 2.600 6.000 -2.600
25 2.400 9.000 -2.400
26 2.200 12.000 -2.200
27 2.000 15.000 -2.000
28 1.800 18.000 -1.800
29 1.600 21.000 -1.600
30 1.400 24.000 -1.400
31 -3.000 0.000 -3.000
32 -1.200 27.000 -1.200
33 -2.800 3.000 -2.800
34 -2.600 6.000 -2.600
35 -2.400 9.000 -2.400
36 -2.200 12.000 -2.200
37 -2.000 15.000 -2.000
38 -1.800 18.000 -1.800
16
39 -1.600 21.000 -1.600
40 -1.400 24.000 -1.400
41 1.200 30.000 1.200
42 -1.200 30.000 1.200
43 1.200 30.000 -1.200
44 -1.200 30.000 -1.200
45 4.200 27.000 1.200
46 7.200 27.000 1.200
47 4.200 30.000 1.200
48 4.200 27.000 -1.200
49 7.200 27.000 -1.200
50 4.200 30.000 -1.200
51 -4.200 27.000 1.200
52 -7.200 27.000 1.200
17
53 -4.200 30.000 1.200
54 -4.200 27.000 -1.200
55 -7.200 27.000 -1.200
56 -4.200 30.000 -1.200
57 1.200 33.000 1.200
58 -1.200 33.000 1.200
59 1.200 33.000 -1.200
60 -1.200 33.000 -1.200
61 0.000 35.000 0.000
MEMBER INCIDENCES
1 1 3
2 3 4
3 4 5
4 5 6
18
5 6 7
6 7 8
7 8 9
8 9 10
9 10 2
10 11 13
11 13 14
12 14 15
13 15 16
14 16 17
15 17 18
16 18 19
17 19 20
18 20 12
19
19 13 3
20 14 4
21 15 5
22 16 6
23 17 7
24 18 8
25 19 9
26 20 10
27 12 2
28 11 3
29 1 13
30 13 4
31 3 14
20
32 14 5
33 15 4
34 15 6
35 16 5
36 16 7
37 17 6
38 17 8
39 18 7
40 18 9
41 19 8
42 19 10
43 20 9
44 20 2
21
45 12 10
46 21 23
47 23 24
48 24 25
49 25 26
50 26 27
51 27 28
52 28 29
53 29 30
54 30 22
55 3 23
56 4 24
57 5 25
22
58 6 26
59 7 27
60 8 28
61 9 29
62 10 30
63 2 22
64 1 23
65 21 3
66 3 24
67 23 4
68 4 25
69 5 24
70 5 26
71 6 25
23
72 6 27
73 7 26
74 7 28
75 8 27
76 8 29
77 9 28
78 9 30
79 10 29
80 10 22
81 2 30
82 31 33
83 33 34
84 34 35
24
85 35 36
86 36 37
87 37 38
88 38 39
89 39 40
90 40 32
91 23 33
92 24 34
93 25 35
94 26 36
95 27 37
96 28 38
97 29 39
25
98 30 40
99 22 32
100 21 33
101 31 23
102 23 34
103 33 24
104 24 35
105 25 34
106 25 36
107 26 35
108 26 37
109 27 36
26
110 27 38
111 28 37
112 28 39
113 29 38
114 29 40
115 30 39
116 30 32
117 22 40
118 33 13
119 34 14
120 35 15
27
121 36 16
122 37 17
123 38 18
124 39 19
125 40 20
126 32 12
127 31 13
128 11 33
129 33 14
130 13 34
131 34 15
28
132 35 14
133 35 16
134 36 15
135 36 17
136 37 16
137 37 18
138 38 17
139 38 19
140 39 18
141 39 20
142 40 19
29
143 40 12
144 32 20
145 32 44
146 12 42
147 2 41
148 22 43
149 42 41
150 41 43
151 43 44
152 44 42
153 12 41
154 42 2
155 22 41
30
156 43 2
157 43 32
158 44 22
159 12 44
160 32 42
161 41 47
162 47 45
163 45 2
164 47 46
165 46 45
166 41 45
167 43 50
168 50 48
31
169 48 22
170 50 49
171 49 48
172 43 48
173 47 50
174 46 49
175 45 48
176 41 50
177 50 46
178 43 47
179 47 49
180 22 50
181 2 47
32
182 22 45
183 2 48
184 47 48
185 50 45
186 45 49
187 48 46
188 42 53
189 53 51
190 51 12
191 53 52
192 52 51
193 42 51
194 44 56
33
195 56 54
196 54 32
197 56 55
198 55 54
199 44 54
200 53 56
201 52 55
202 51 54
203 42 56
204 56 52
34
205 44 53
206 53 55
207 32 56
208 12 53
209 32 51
210 12 54
211 53 54
212 56 51
213 51 55
214 54 52
215 44 60
216 42 58
35
217 41 57
218 43 59
219 60 59
220 59 57
221 57 58
222 58 60
223 44 58
224 42 60
225 42 57
36
226 41 58
227 44 59
228 43 60
229 43 57
230 41 59
231 60 57
232 59 58
235 33 3
236 13 23
237 34 4
238 14 24
37
239 35 5
240 15 25
241 36 6
242 16 26
243 37 7
244 17 27
245 38 8
246 18 28
247 39 9
248 19 29
249 40 10
250 20 30
38
251 32 2
252 22 12
253 44 41
254 43 42
255 60 61
256 58 61
257 57 61
258 59 61
MEMBER PROPERTY INDIAN
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1 TO 18 46 TO 54 82 TO 90 145 TO 148 215 TO 218 TABLE LD ISA200X150X18 SP 0.01
19 TO 26 28 TO 45 55 TO 62 64 TO 81 91 TO 98 100 TO 125 TABLE ST ISA150X150X10
127 TO 144 155 156 159 160 223 224 229 230 235 TO 250 TABLE ST ISA150X150X10
27 63 99 126 149 TO 154 157 158 161 TO 214 219 TO 222 TABLE ST ISA80X50X6
225 TO 228 231 232 251 TO 258 TABLE ST ISA80X50X6
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UNIT MMS NEWTON
DEFINE MATERIAL START
ISOTROPIC STEEL
E 205000
POISSON 0.3
DENSITY 7.68195e-005
ALPHA 1.2e-005
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DAMP 0.03
END DEFINE MATERIAL
UNIT METER KN
CONSTANTS
MATERIAL STEEL MEMB 1 TO 232 235 TO 258
SUPPORTS
1 11 21 31 FIXED
UNIT METER KG
LOAD 1 VERT
42
SELFWEIGHT Y -1
JOINT LOAD
61 FX 732
46 49 52 55 FX 153
61 FX 1280 FY -1016 FZ 160
43
46 49 52 55 FX 9006 FY -7844 FZ 1968
2 12 22 32 FX 4503 FY -3937 FZ 1968
LOAD 2 GWBC
SELFWEIGHT Y -1
JOINT LOAD
61 FX 549
46 49 52 55 FX 1148
61 FX 515 FY -762 FZ 2342
44
46 49 52 55 FX 6755 FY -5906
2 12 22 32 FX 3378 FY -2953
LOAD 3 LEFT PCBC
SELFWEIGHT Y -1
45
JOINT LOAD
61 FX 549
46 49 52 55 FX 1148
61 FX 960 FY -762
46 49 FX 6755 FY -5906
52 55 FX 4211 FY -4551 FZ 13293
2 12 22 32 FX 3378 FY -2953
LOAD 4 RIGHT PCBC
SELFWEIGHT Y -1
JOINT LOAD
61 FX 549
46 49 52 55 FX 1148
61 FX 960 FY -762
52 55 FX 6755 FY -5906
46 49 FX 4211 FY -4551 FZ 13293
46
2 12 22 32 FX 3378 FY -2953
PERFORM ANALYSIS
UNIT MMS NEWTON
PARAMETER
CODE IS802
LY 2800 MEMB 28
47
LZ 2800 MEMB 28
MAIN 1 MEMB 1
ELA 4 ALL
CNSF 1 ALL
DBL 16 ALL
GUSSET 8 ALL
TRACK 9 ALL
CHECK CODE ALL
PERFORM ANALYSIS
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PRINT SUPPORT REACTION
FINISH
************************************************************************
*Atul Saxena
*Size of Bolts is calculated. This file may be exported to Tekla Structures and detailed in Tekla.
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NOTES::
*First copy and paste this input file in your staad input file browser. Run analysis and get out put file Note that file to be imported shoud be in .std format. Genarally in staad all members of same group are separated by hyphens. We have to replace
*Will size of bolts and nos will automatically reflected in Tekla Structures??
*Basically in the staad input there is a concept of grouping the members with similar characteristics such as member property, constants or loads in one go. So at the end of that particular group the member property is defined whereas at the end of each line in that group definition a hyphen *can be seen which indicates the continuation of that particular group. *So this hyphen has to be replaced by the member property at the end of each and every line for all groups before importing the same into Tekla *Structures and if there is any user defined c/s given as an input in staad then the same needs to be taken care in Tekla Structures by defining a *conversion file or revising the profile catalog.
