Mechanical APDL Basic Analysis Guide - Ansys
Mechanical APDL Basic Analysis Guide - Ansys Mechanical APDL Basic Analysis Guide - Ansys
Chapter 2: Loading Figure 2.10 Tapered Load on a Cylindrical Shell You might be tempted to use 270°, instead of -90°, for SLZER: SFGRAD,PRES,11,Y,270,1 ! Slope the pressure in the theta direction ! of C.S. 11. Specified pressure in effect ! at 270°, tapering at 1 unit per degree SF,ALL,PRES,400 ! Pressure at all selected nodes: ! 400 at -90°, 490 at 0°, 580 at +90° However, as shown on the left in Figure 2.11 (p. 38), this will result in a tapered load much different than intended. This is because the singularity is still located at 180° (the θ coordinates still range from -90° to +90°), but SLZER is not between -180° and +180°. As a result, the program will use a load value of 400 at 270°, and a slope of 1 unit per degree to calculate the applied load values of 220 at +90°, 130 at 0°, and 40 at -90°. You can avoid this behavior by following the second guideline, that is, choosing SLZER to be between ±180° when the singularity is at 180°, and between 0° and 360° when the singularity is at 0°. Figure 2.11 Violation of Guideline 2 (left) and Guideline 1 (right) 220 +90° y 11 x 310 +180° 0° 130 -90° +270° 40 400 310 +180° 220 +90° y 11 +270° 400 x 0° +360° singularity 130 490 Suppose that you change the singularity location to 0°, thereby satisfying the second guideline (270° is then between 0° and 360°). But then the θ coordinates of the nodes range from 0° to +90° for the upper half of 38 Release 13.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information of ANSYS, Inc. and its subsidiaries and affiliates.
the shell, and 270° to 360° for the lower half. The surface to be loaded crosses the singularity, a violation of Guideline 1: CSCIR,11,1 ! Change singularity to 0° SFGRAD,PRES,11,Y,270,1 ! Slope the pressure in the theta direction ! of C.S. 11. Specified pressure in effect ! at 270°, tapering at 1 unit per degree SF,ALL,PRES,400 ! Pressure at all selected nodes: ! 400 at 270°, 490 at 360°, 220 at +90° ! and 130 at 0° Again the program will use a load value of 400 at 270° and a slope of 1 unit per degree to calculate the applied load values of 400 at 270°, 490 at 360°, 220 at 90°, and 130 at 0°. Violating Guideline 1 will cause a singularity in the tapered load itself, as shown on the right in Figure 2.11 (p. 38). Due to node discretization, the actual load applied will not change as abruptly at the singularity as it is shown in the figure. Instead, the node at 0° will have the load value of, in the case shown, 130, while the next node clockwise (say, at 358°) will have a value of 488. Note The SFGRAD specification stays active for all subsequent load application commands. To remove the specification, simply issue SFGRAD without any arguments. Also, if an SFGRAD specification is active when a load step file is read, the program erases the specification before reading the file. Large deflection effects can change the node locations significantly. The SFGRAD slope and load value calculations, which are based on node locations, are not updated to account for these changes. If you need this capability, use SURF153 with face 3 loading or SURF154 with face 4 loading. 2.5.7.4. Repeating a Surface Load By default, if you repeat a surface load at the same surface, the new specification replaces the previous one. You can change this default to add (for accumulation) or ignore using one of the following: Command(s): SFCUM GUI: Main Menu> Preprocessor> Loads> Define Loads> Settings> Replace vs. Add> Surface Loads Main Menu> Solution> Define Loads> Settings> Replace vs. Add> Surface Loads Any surface load you set stays set until you issue another SFCUM command. To reset the default setting (replacement), simply issue SFCUM without any arguments. The SFSCALE command allows you to scale existing surface load values. Both SFCUM and SFSCALE act only on the selected set of elements. The Lab field allows you to choose the surface load label. 2.5.7.5. Transferring Surface Loads To transfer surface loads that have been applied to the solid model to the corresponding finite element model, use one of the following: Command(s): SFTRAN GUI: Main Menu> Preprocessor> Loads> Define Loads> Operate> Transfer to FE> Surface Loads Main Menu> Solution> Define Loads> Operate> Transfer to FE> Surface Loads To transfer all solid model boundary conditions, use the SBCTRAN command. (See DOF Constraints (p. 27) for a description of DOF constraints.) Release 13.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information of ANSYS, Inc. and its subsidiaries and affiliates. 2.5.7. Surface Loads 39
- Page 3 and 4: Table of Contents 1. Getting Starte
- Page 5 and 6: 2.8.4.3. Define Material Properties
- Page 7 and 8: 7.2.1.6. Particle Flow and Charged
- Page 9 and 10: 10. Getting Started with Graphics .
- Page 11 and 12: 13.2.4.1.Turning Load Symbols and C
- Page 13 and 14: 20.8. Reviewing Contents of Binary
- Page 15 and 16: List of Tables 2.1. DOF Constraints
- Page 17 and 18: Chapter 1: Getting Started with ANS
- Page 19 and 20: shown below define two element type
- Page 21 and 22: You can choose constant, isotropic,
- Page 23 and 24: You can save linear material proper
- Page 25 and 26: Figure 1.4 Material Model Interface
- Page 27 and 28: Figure 1.7 Data Input Dialog Box -
- Page 29 and 30: The first example below is intended
- Page 31 and 32: 9. Click on OK. The dialog box clos
- Page 33 and 34: 1.1.4.9. Reading a Material Library
- Page 35 and 36: If you are performing a static or f
- Page 37 and 38: Chapter 2: Loading The primary obje
- Page 39 and 40: Figure 2.2 Transient Load History C
- Page 41 and 42: The arc-length method is an advance
- Page 43 and 44: • Transferred solid loads will re
- Page 45 and 46: Note If the node rotation angles th
- Page 47 and 48: Figure 2.7 Scaling Temperature Cons
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- Page 51 and 52: Utility Menu> List> Loads> Surface>
- Page 53: Figure 2.9 Example of Surface Load
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- Page 59 and 60: Figure 2.15 Transfers to BFK Loads
- Page 61 and 62: CASE C: At least one BFV, BFA, or B
- Page 63 and 64: A handy way to specify density so t
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- Page 71 and 72: 2.6. Specifying Load Step Options A
- Page 73 and 74: - All loads changed in later load s
- Page 75 and 76: Main Menu> Preprocessor> Loads> Loa
- Page 77 and 78: Command GUI Menu Paths Main Menu> S
- Page 79 and 80: ! Load Step 1: D, ... ! Loads SF, .
- Page 81 and 82: Modeling> Create> Elements> Auto Nu
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- Page 87 and 88: 11. Select Utility Menu> PlotCtrls>
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the shell, and 270° to 360° for the lower half. The surface to be loaded crosses the singularity, a violation of<br />
<strong>Guide</strong>line 1:<br />
CSCIR,11,1 ! Change singularity to 0°<br />
SFGRAD,PRES,11,Y,270,1 ! Slope the pressure in the theta direction<br />
! of C.S. 11. Specified pressure in effect<br />
! at 270°, tapering at 1 unit per degree<br />
SF,ALL,PRES,400 ! Pressure at all selected nodes:<br />
! 400 at 270°, 490 at 360°, 220 at +90°<br />
! and 130 at 0°<br />
Again the program will use a load value of 400 at 270° and a slope of 1 unit per degree to calculate the<br />
applied load values of 400 at 270°, 490 at 360°, 220 at 90°, and 130 at 0°. Violating <strong>Guide</strong>line 1 will cause a<br />
singularity in the tapered load itself, as shown on the right in Figure 2.11 (p. 38). Due to node discretization,<br />
the actual load applied will not change as abruptly at the singularity as it is shown in the figure. Instead,<br />
the node at 0° will have the load value of, in the case shown, 130, while the next node clockwise (say, at<br />
358°) will have a value of 488.<br />
Note<br />
The SFGRAD specification stays active for all subsequent load application commands. To remove<br />
the specification, simply issue SFGRAD without any arguments. Also, if an SFGRAD specification<br />
is active when a load step file is read, the program erases the specification before reading the<br />
file.<br />
Large deflection effects can change the node locations significantly. The SFGRAD slope and load value calculations,<br />
which are based on node locations, are not updated to account for these changes. If you need<br />
this capability, use SURF153 with face 3 loading or SURF154 with face 4 loading.<br />
2.5.7.4. Repeating a Surface Load<br />
By default, if you repeat a surface load at the same surface, the new specification replaces the previous one.<br />
You can change this default to add (for accumulation) or ignore using one of the following:<br />
Command(s): SFCUM<br />
GUI: Main Menu> Preprocessor> Loads> Define Loads> Settings> Replace vs. Add> Surface Loads<br />
Main Menu> Solution> Define Loads> Settings> Replace vs. Add> Surface Loads<br />
Any surface load you set stays set until you issue another SFCUM command. To reset the default setting<br />
(replacement), simply issue SFCUM without any arguments. The SFSCALE command allows you to scale<br />
existing surface load values. Both SFCUM and SFSCALE act only on the selected set of elements. The Lab<br />
field allows you to choose the surface load label.<br />
2.5.7.5. Transferring Surface Loads<br />
To transfer surface loads that have been applied to the solid model to the corresponding finite element<br />
model, use one of the following:<br />
Command(s): SFTRAN<br />
GUI: Main Menu> Preprocessor> Loads> Define Loads> Operate> Transfer to FE> Surface Loads<br />
Main Menu> Solution> Define Loads> Operate> Transfer to FE> Surface Loads<br />
To transfer all solid model boundary conditions, use the SBCTRAN command. (See DOF Constraints (p. 27)<br />
for a description of DOF constraints.)<br />
Release 13.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information<br />
of ANSYS, Inc. and its subsidiaries and affiliates.<br />
2.5.7. Surface Loads<br />
39