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Envelope example

 
These document attempts to bring to user, a easy going way of controlling the envelope utility. That is the reason why the examples ahead has been performed. In first, an example with the Totals max/min envelope type will be shaped.
 
The example consists of a beam 2 meters long made out of steel and a IPE 220 section:
 
 
The applied loads will be specified ahead:
 
 
The beam is double and simply supported, respectively, in its endings.
 
 
Three different load cases are defined, adding the LoadGroup_1 in the first Load Case, the LoadGroup_2 in the second Load case and the LoadGroup_3 in the third one. After solving, we use the Envelope utility:
 
 
The three Load Cases are attached and the Envelope type is shaped with the detailed information on the image from above. In this example maximum absolute values in movements, minimum absolute values in stresses and strains and maximum values in bending and moments, will be applied on the envelope.
 
For this purpose: movements, von misses and bending moments; will be visualized ahead:
 
Movements:
The envelope has been shaped from the maximum values of the amount of load states, obtaining the results ahead:
 
Bending moment in Z axis:
 
The envelope has been shaped from the maximum values of the amount of load states, obtaining the results ahead:
 
Von mises equivalent stress:
 
The envelope has been shaped from the maximum values of the amount of load states, obtaining the results ahead:
 
We are comparing the Von mises equivalent stresses in the first IP, therefore this table with the Von mises values in the first IP, for all the previous cases, will be visualized:
 
Structural Element
Element
Node
End
At IP 0 Load_1
At IP 0 Load_2
At IP 0 Load_3
At IP 0 MaxMin_Envelope
 
 
 
 
MPa
MPa
MPa
MPa
Beam
1
1
0
1479.949
1151.071
822.194
822.194
Beam
1
2
1
5523.244
4295.856
3068.469
3068.469
Beam
2
2
0
8154.264
6597.999
4712.857
4712.857
Beam
2
3
1
11299.049
9742.783
6959.132
6959.132
Beam
3
3
0
13272.314
12044.927
8603.519
8603.519
Beam
3
4
1
15518.589
15189.712
10849.794
10849.794
Beam
4
4
0
16834.099
15847.467
12494.181
12.494.181
Beam
4
5
1
18181.863
14499.702
14740.456
14499.702
Beam
5
5
0
18839.620
13513.070
16384.844
13513.070
Beam
5
6
1
19288.875
12165.304
18631.119
12165.304
Beam
6
6
0
19288.875
11178.671
20275.507
11178.671
Beam
6
7
1
18839.620
9830.907
22521.782
9830.907
Beam
7
7
0
18181.863
8844.274
24166.169
8844.274
Beam
7
8
1
16834.099
7496.509
26412.444
7496.509
Beam
8
8
0
15518.589
6509.876
10849.794
6509.876
Beam
8
9
1
13272.314
5162.111
8603.519
5162.111
Beam
9
9
0
11299.049
4175.479
6959.132
4175.479
Beam
9
10
1
8154.264
2827.714
4712.857
2827.714
Beam
10
10
0
5523.244
1841.081
3068.469
1841.081
Beam
10
11
1
1479.949
493.316
822.194
493.316
 
As it can be seen, the envelope has been shaped from the minimum values of the amount of load states.
 
Once the example carrying out the Totals max/min envelope type, we will branch into the example with the Concomitant envelope type. The same structure has been taking, even materials, sections and loads, giving rise to the same load states. However, this load states will deal with the concomitant option. The algorithm of this option will perform the results attending to a criterion for a specific option from the forces and moments drop down.
 
 
In relation to this example, we are looking for the maximum values of the Bending moment about the local Z-axis. The envelope for this result type, will be shaped taking the maximum moments from the whole amount of load states, for every element. The concomitant reactions would be those which led to these maximum bending moment. That is the reason why the rest of the forces and moments results will be shaped from these concomitant results.
 
Bending moment in Z axis:
 
Maybe plots are a bit difficult to read into. Nevertheless, table results pretend to be more intuitive and easy going as a result of get the concept properly well.
 
Structural Element
Element
Node
End
Z-BendMoment L1
Z-BendMoment L2
Z-BendMoment L3
Z-BendMoment Envelope
 
 
 
 
kN·m
kN·m
kN·m
kN·m
Beam
1
1
0
0.000
0.000
0.000
0.000
Beam
1
2
1
1.800.000
1400.000
1000.000
1800.000
Beam
2
2
0
1800.000
1400.000
1000.000
1800.000
Beam
2
3
1
3200.000
2800.000
2000.000
3200.000
Beam
3
3
0
3200.000
2800.000
2000.000
3200.000
Beam
3
4
1
4200.000
4200.000
3000.000
4200.000
Beam
4
4
0
4200.000
4200.000
3000.000
4200.000
Beam
4
5
1
4800.000
3600.000
4000.000
4800.000
Beam
5
5
0
4800.000
3600.000
4000.000
4800.000
Beam
5
6
1
5000.000
3000.000
5000.000
5000.000
Beam
6
6
0
5000.000
3000.000
5000.000
5000.000
Beam
6
7
1
4800.000
2400.000
6000.000
6000.000
Beam
7
7
0
4800.000
2400.000
6000.000
6000.000
Beam
7
8
1
4200.000
1800.000
7000.000
7000.000
Beam
8
8
0
4200.000
1800.000
-3000.000
4200.000
Beam
8
9
1
3200.000
1200.000
-2000.000
3200.000
Beam
9
9
0
3200.000
1200.000
-2000.000
3200.000
Beam
9
10
1
1800.000
600.000
-1000.000
1800.000
Beam
10
10
0
1800.000
600.000
-1000.000
1800.000
Beam
10
11
1
0.000
0.000
0.000
0.000
 
As it can be seen, maximum values for every element, in relation to the Bending moment in the local Z axis, have been taken into account when the concomitant envelope has been processed. The rest of the results would be shaped with the concomitant values.