plane stress bracket tut
TRANSCRIPT
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Tutorials | Chapter 2. Structural Tutorial |
2.1. Static Analysis of a Corner Bracket
2.1.1. Problem Specification
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2.1.2. Problem Description
This is a simple, single load step, structural static analysis of the corner angle bracket shown below. The upper left-hand pin hole is
constrained (welded) around its entire circumference, and a tapered pressure load is applied to the bottom of the lower right-hand
pin hole. The objective of the problem is to demonstrate the typical ANSYS analysis procedure. The US Customary system of units
is used.
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2.1.2.1. Given
The dimensions of the corner bracket are shown in the accompanying figure. The bracket is made of A36 steel with a Young’s
modulus of 30E6 psi and Poisson’s ratio of .27.
2.1.2.2. Approach and Assumptions
Assume plane stress for this analysis. Since the bracket is thin in the z direction (1/2 inch thickness) compared to its x and
dimensions, and since the pressure load acts only in the x-y plane, this is a valid assumption.
Your approach is to use solid modeling to generate the 2-D model and automatically mesh it with nodes and elements.
(Another alternative in ANSYS is to create the nodes and elements directly.)
2.1.2.3. Summary of Steps
Use the information in the problem description and the steps below as a guideline in solving the problem on your own. Or, use the
detailed interactive step-by-step solution by choosing the link for step 1.
Note
If your system includes a Flash player (from
Macromedia, Inc.), you can view
demonstration videos of each step by
pointing your web browser to the followingURL
address:http://www.ansys.com/techmedia/structural_tutorial_vid
eos.html.
Build Geometry
1Define rectangles.
2Change plot controls and replot.
3Change working plane to polar and create first circle.
4Move working plane and create second circle.
5Add areas.
6Create line fillet.
7Create fillet area.8Add areas together.
9Create first pin hole.
10Move working plane and create second pin hole.
11Subtract pin holes from bracket.
12Save the database as model.db.
Define Materials
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1Set Preferences.
2Define Material Properties.
3Define element types and options.
4Define real constants.
Generate Mesh
17. Mesh the area.
18. Save the database as mesh.db.
Apply Loads 19. Apply displacement constraints. 20. Apply pressure
load.
Back To TopObtain Solution
21. Solve.
Review Results
1Enter the general postprocessor and read in the results.2Plot the deformed shape.
3Plot the von Mises equivalent stress.
4List the reaction solution.5Exit the ANSYS program.
2.1.3. Build Geometry
This is the beginning of Preprocessing.
2.1.3.1. Step 1: Define rectangles.
There are several ways to create the model geometry within
ANSYS, some more convenient than others. The first step is
to recognize that you can construct the bracket easily with
combinations of rectangles and circle Primitives.
Decide where the origin will be located and then define the
rectangle and circle primitives relative to that origin. The
location of the origin is arbitrary. Here, use the center of the
upper left-hand hole. ANSYS does not need to know where the
origin is. Simply begin by defining a rectangle relative to that
location. In ANSYS, this origin is called the global origin.1Main Menu> Preprocessor> Modeling> Create> Areas>
Rectangle> By Dimensions
2Enter the following:
X1 = 0
(Note: Press the Tab key betweenentries)
X2 = 6
Y1 = -1
Y2 = 1
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5a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4
850202000000000000000000000000000000000
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000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b7074000002040000
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0000
13. Apply to create the first
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000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c40
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rectangle.
Enter the following: X1 = 4 X2 = 6 Y1 = -1
OK to create the second rectangle and close the dialog box.
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00000
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2.1.3.2. Step 2: Change plot controls and replot.
The area plot shows both rectangles, which are areas, in the
same color. To more clearly distinguish between areas, turn on
area numbers and colors. The "Plot Numbering Controls" dialog
box on the Utility Menu controls how items are displayed in theGraphics Window. By default, a "replot" is automatically
performed upon execution of the dialog box. The replot
operation will repeat the last plotting operation that occurred (inthis case, an area plot).
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000000000000000000000000000000000000000000000000000
000000000000000000000000116370727400000150000000336
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00000000000000000000000000000000
memory to the ANSYS database. Tosave thatdatabase to a file, use the SAVE operation,
available as a tool on the Toolbar. ANSYS
names the database file using the format jobname.db. If you started ANSYS using the
product launcher, you can specify a jobname at
that point (the default jobname is file). You cancheck the current jobname at any time by
choosing Utility Menu> List> Status> Global
Status. You can also save the database at
specific milestone points in the analysis(suchas after the model is complete, orafter themodel is meshed) bychoosing Utility Menu>
File> Save As and specifying different
jobnames (model.db, or mesh.db, etc.).
It is important to do an occasional save so thatif you make a mistake, you can restore the
model from the last saved state. You restore
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the model using the RESUME operation, also
available on the Toolbar. (Youcan also find
SAVE and RESUMEon the Utility Menu,
under File.)
4. Toolbar: SAVE_DB.
2.1.3.3. Step 3: Change working plane to polar andcreate first circle.
The next step in the model construction is to create the half
circle at each end of the bracket. You will actually create a full
circle on each end and then combine the circles and rectangles
with a Boolean "add" operation (discussed in step 5.). To create
the circles, you will use and display the working plane. You
could have shown the working plane as you created the
rectangles but it was not necessary.
Before you begin however, first "zoom out" within the
Graphics Window so you can see more of the circles as you
create them. You do this using the "Pan-Zoom-Rotate" dialog box, a convenient graphics control box you’ll use often in any
ANSYS session.
1Utility Menu> PlotCtrls> Pan, Zoom, Rotate
2Click on small dot once to zoom out.
3Close dialog box.
4Utility Menu> WorkPlane> Display Working Plane (toggle
on)
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00000
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Notice the working plane origin is immediatelyplotted in the Graphics Window. It is indicatedby the WX and WY symbols; right nowcoincident with the global origin X and Ysymbols. Next you will change the WP type topolar, change the snap increment, anddisplay the grid.
61Utility Menu> WorkPlane> WP Settings
2Click on Polar.
3Click on Grid and Triad.
4Enter .1 for snap increment.5OK to define settings and close the dialog box.
6Main Menu> Preprocessor> Modeling> Create> Areas>
Circle> Solid Circle
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00000
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00000
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00000
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0000
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Be sure to read prompt before picking.
81. 11. Pick center point at:
9 WP X = 0 (in Graphics Window shown below) WP Y = 02Move mouse to radius of 1 and click left button to create circle.3OK to close picking menu.
4Toolbar: SAVE_DB.
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000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000
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6
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500000003364657363000001840000006c77747
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0000
7 Note
8While you are positioning the cursor for picking, the
"dynamic" WP X and Y values are displayed in the
Solid Circular Area dialog box. Also, as an alternative
to picking, you can type these values along with the
radius into the dialog box.
2.1.3.4. Step 4: Move working plane and create second
circle.To create the circle at the other end of the bracket in the same
manner, you need to first move the working plane to the origin
of the circle. The simplest way to do this without entering
number offsets is to move the WP to an average keypoint
location by picking the keypoints at the bottom corners of thlower, right rectangle.
1Utility Menu> WorkPlane> Offset WP to> Keypoints
2Pick keypoint at lower left corner of rectangle.
3Pick keypoint at lower right of rectangle.
4OK to close picking menu.5Main Menu> Preprocessor> Modeling> Create> Areas>
Circle> Solid Circle
6Pick center point at: WP X = 0 WP Y = 0
7Move mouse to radius of 1 and click left button to create circle
8OK to close picking menu.
9Toolbar: SAVE_DB.10
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00000
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 15/51
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0000112.1.3.5. Step 5: Add areas.
Now that the appropriate pieces of the model are defined
(rectangles and circles), you need to add them together so the
model becomes one continuous piece. You do this with the
Boolean add operation for areas.
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00000000000000000000000000000000
2.1.3.6. Step 6: Create line fillet.
1Utility Menu> PlotCtrls> Numbering
2Turn on line numbering.3OK to change controls, close
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 16/51
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the dialog box, and automatically replot.
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0000
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 17/51
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00004. Utility Menu> WorkPlane> Display Working Plane
(toggle off)
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000006. Pick lines 17 and 8.
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00000
1OK to finish picking lines (in picking menu).
2Enter .4 as the radius.
3OK to create line fillet and close the dialog box.4Utility Menu> Plot> Lines
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 18/51
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0000
2.1.3.7. Step 7: Create fillet area.
1Utility Menu> PlotCtrls> Pan, Zoom, Rotate
2Click on Zoom button.
3Move mouse to fillet region, click left button, move mouse out
and click again.
4Main Menu> Preprocessor> Modeling> Create> Areas>
Arbitrary> By Lines
5Pick lines 4, 5, and 1.
6OK to create area and close the picking menu.
7Click on Fit button.8Close the Pan, Zoom, Rotate dialog box.
9Utility Menu> Plot> Areas
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 19/51
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 20/51
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 21/51
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10. Toolbar: SAVE_DB.
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00000000000000000000000000000000
2.1.3.8. Step 8: Add areas together.
1Main Menu> Preprocessor> Modeling> Operate>
Booleans> Add> Areas
2Pick All for all areas to be added.
3Toolbar: SAVE_DB.
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0000
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00000
2.1.3.9. Step 9: Create first pin hole.
1Utility Menu> WorkPlane> Display Working Plane (toggleon)2Main Menu> Preprocessor> Modeling> Create> Areas>
Circle> Solid Circle
3Pick center point at:WP X = 0 (in Graphics Window) WP Y =
0
4Move mouse to radius of .4 (shown in the picking menu) andclick left button to create circle.
5OK to close picking menu.
67 ffd8ffe000104a46494600010201006000600000ffe20c584943435f50524f46494c450001010000
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82.1.3.10. Step 10: Move working plane and create
second pin hole.1Utility Menu> WorkPlane> Offset WP to> Global Origin
2Main Menu> Preprocessor> Modeling> Create> Areas>
Circle> Solid Circle
3Pick center point at: WP X = 0 (in Graphics Window) WP Y =
0
4Move mouse to radius of .4 (shown in the picking menu) and
click left mouse button to create circle.
5OK to close picking menu.
6Utility Menu> WorkPlane> Display Working Plane (toggle
off)
7Utility Menu> Plot> Replot
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000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747
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9From this area plot, it appears that one of the pin hole areasis not there. However, it is there (as indicated by the
presence of its lines), you just can't see it in the final display
of the screen. That is because the bracket area is drawn on
top of it. An easy way to see all areas is to plot the lines
instead.
1Utility Menu> Plot> Lines
2Toolbar: SAVE_DB.
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42.1.3.11. Step 11: Subtract pin holes from bracket.
1Main Menu> Preprocessor> Modeling> Operate>
Booleans> Subtract> Areas
2Pick bracket as base area from which to subtract.
3Apply (in picking menu).
4Pick both pin holes as areas to be subtracted.
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5. OK to subtract holes and close picking menu.
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2.1.3.12. Step 12: Save the database as model.db.
At this point, you will save the database to a named file -- a
name that represents the model before meshing. If you decide to
go back and remesh, you'll need to resume this database file.
You will save it as model.db.
1Utility Menu> File> Save As
2Enter model.db for the database file name.
3OK to save and close dialog box.
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00000000000000000000000000000000
2.1.4. Define Materials
2.1.4.1. Step 13: Set preferences.
In preparation for defining materials, you will set preferences so
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that only materials that pertain to a structural analysis are
available for you to choose.
To set preferences:
1Main Menu>
Preferences
2Turn onstructural filtering. The options may differ from what is
shown heresince they depend on the
ANSYS product
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you are using.
3. OK to applyfiltering and close the dialog
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box.
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dialog box.
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6. Material> Exit
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000002.1.4.3. Step 15: Define element types and options.
In any analysis, you need to select from a library of element
types and define the appropriate ones for your analysis.
For this analysis, you will use only one element type, PLANE82,
which is a 2-D, quadratic, structural, higher-order element. The
choice of a higher-order element here allows you to have a
coarser mesh than with lower-order elements while still
maintaining solution accuracy. Also, ANSYS will generate som
triangle shaped elements in the mesh that would otherwise be
inaccurate if you used lower-order elements (PLANE42). You
will need to specify plane stress with thickness as an option for
PLANE82. (You will define the thickness as a real constant in
the next step.)
1Main Menu> Preprocessor>
Element Type>
Add/Edit/Delete
2Add an element type.
3. Structural solid family of
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elements. 4. Choose the 8-node quad
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(PLANE82). 5. OK to apply the element type
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and close the dialog box. 6.Options for
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PLANE82 are to be defined.
1. 7. Choose plane stress withthickness option for elementffd8ffe000104a46494600010201004800480000ffe20c58494343
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0000000000000000000000000000000 behavior.3OK to specify options and close the optionsdialog box.
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9. Close the element type dialog
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box.
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0000000000000000000000000000000000000000000
2.1.4.4. Step 16: Define real constants.
For this analysis, since the assumption is plane stress with
thickness, you will enter the thickness as a real constant for PLANE82. To find out more information about PLANE82, you
will use the ANSYS Help System in this step by clicking on a
Help button from within a dialog box.
1Main Menu>
Preprocessor> Real
Constants>Add/Edit/Delete
2Add a real constant set.
3OK for PLANE82.
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ffd8ffe000104a46494600010201004800480000
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Before clicking on the Help button in the nextstep, you should be aware that the help
information may appear in the same window as
this tutorial, replacing the contents of the tutorial.After reading the help information, click on the
Back button to return to this tutorial. If the help
information appears in a separate window from
the tutorial, minimize or close the help windowafter you read the help information.
14. Help to get help on
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PLANE82.
Hold left mouse button down to scroll through element
description.If the help information replaced the tutorial, click on the Back
button to return to the tutorial.
Enter .5 for THK.
1. 8. OK to define the real
constant and close the dialog box.
2Close the real constant dialog box.
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0000
2.1.5. Generate Mesh
2.1.5.1. Step 17: Mesh the area.
One nice feature of the ANSYS program is that you can
automatically mesh the model without specifying any mesh size
controls. This is using what is called a default mesh. If you’re
not sure how to determine the mesh density, let ANSYS try it
first! Meshing this model with a default mesh however,
generates more elements than are allowed in the ANSYS ED
program. Instead you will specify a global element size to
control overall mesh density.
1Main Menu>
Preprocessor> Meshing>Mesh Tool
2Set Global Size control.
3Type in 0.5.
4OK.
5Choose Area Meshing.
6Click on Mesh.
7Pick All for the area to be meshed (in picking menu). Close an
warning messages that appear.8Close the Mesh Tool.
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Note
The mesh you see on your screen may vary slightly
from the mesh shown here. As a result of this, you maysee slightly different results during postprocessing. For
a discussion of results accuracy, see Planning Your
Approach in the ANSYS Modeling and Meshing Guide.
2.1.5.2. Step 18: Save the database as mesh.db.
Here again, you will save the database to a named file, this time
mesh.db.
1Utility Menu> File> Save as
2Enter mesh.db for database file name.
3OK to save file and close dialog box.
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00000000000000000000000000000000
2.1.6. Apply Loads
The beginning of the solution phase.
A new, static analysis is the default, so you will not need tospecify analysis type for this problem. Also, there are no
analysis options for this problem.
2.1.6.1. Step 19: Apply displacement constraints.
You can apply displacement constraints directly to lines.
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1Enter 0 for zero displacement.6. OK to apply constraints and close
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dialog box.Utility Menu> Plot Lines
Toolbar: SAVE_DB.
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00000
2.1.6.2. Step 20: Apply pressure load.
Now apply the tapered pressure load to the bottom, right-hand
pin hole. ("Tapered" here means varying linearly.) Note thatwhen a circle is created in ANSYS, four lines define the
perimeter. Therefore, apply the pressure to two lines making upthe lower half of the circle. Since the pressure tapers from a
maximum value (500 psi) at the bottom of the circle to a
minimum value (50 psi) at the sides, apply pressure in two
separate steps, with reverse tapering values for each line.
The ANSYS convention for pressure loading is that a positive
load value represents pressure into the surface (compressive).
1Main Menu> Solution> Define Loads> Apply> Structural>
Pressure> On Lines2Pick line defining bottom left part ofthe circle (line 6).
3Apply.
4Enter 50 for VALUE.
5Enter 500 for optional value.
6Apply.
7Pick line defining bottom right part of circle (line 7).
8Apply.
9Enter 500 for VALUE.
10Enter 50 for optional value.
11OK.
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000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d50
8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 43/51
61636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735
247422049454336313936362d322e31000000000000000000000000000000000000000000000000000000
16ffd8ffe000104a46494600010201006000600000
ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a000
0022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f80000001
46d6561730000040c0000002474656368000004300000000c725452430000043c0000080c67545
2430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000000000000000000000000000000000000000000
00000
2.1.7. Obtain Solution
2.1.7.1. Step 21: Solve.
1Main Menu> Solution> Solve> Current LS
1. 2. Review the information in the status window,
then choose File> Close (Windows), or Close
(X11/Motif), to close the
2. window.23. OK to begin the solution.
1. ffd8ffe000104a46494600010201004800480000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce0002000900060031000061637370
4d5346540000000049454320735247420000000000000000000000000000f 6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c00000014625859
5a0000024000000014646d6e640000
025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000
c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e3100000000000000000000001273524742204945433633936362d322e31000000000000000000000000000000000000000000000000
0000002.3.
ffd8ffe000104a46494600010201004800480000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4
850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a000002400000001464
8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 44/51
6d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c67545
2430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061
636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000000000000000000000000000000000000000000
00000
Choose Yes to any Verify messages that appear.
4. 4. Close the information window when solution is
5.done.
ffd8ffe000104a46494600010201004800480000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5
346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a000
0022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c67545
2430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e31000000000000000000000000000000000000000000000000000000
6.ffd8ffe000104a46494600010201006000600000
ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e7472524742205859
5a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4
850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b7074000002040000
00147258595a00000218000000146758595a000
0022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f80000001
46d6561730000040c0000002474656368000004300000000c725452430000043c0000080c67545
2430000043c0000080c625452430000043c0000080c7465787400000000436f707972696768742
02863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630
000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000000000000000000000000000000000000000000
0000
ANSYS stores the results of this one load step problem in the
database and in the results file, Jobname.RST (or Jobname.RTH
for thermal, Jobname.RMG for magnetic, and Jobname.RFL for
fluid analyses). The database can actually contain only one set o
results at any given time, so in a multiple load step or multiplesubstep analysis, ANSYS stores only the final solution in thedatabase. ANSYS stores all solutions in the results file.
2.1.8. Review Results
The beginning of the postprocessing phase.
Note
8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 45/51
The results you see may vary slightly from what isshown here due to variations in the mesh.
2.1.8.1. Step 22: Enter the general postprocessor and
read in the results.
1. Main Menu> General Postproc> Read Results> Firs
Set
2.1.8.2. Step 23: Plot the deformed shape.
1Main Menu> General Postproc> Plot Results> Deformed
Shape2Choose Def + undeformed.
34 ffd8ffe000104a46494600010201004800480000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a00000240000000146
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
5 3. OK.
6ffd8ffe000104a46494600010201004800480000
ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5
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000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e3100000000000000000000001273524
7422049454336313936362d322e31000000000000000000000000000000000000000000000000000000
ffd8ffe000104a46494600010201005f005f0000f
e20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000
022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d50616
8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 46/51
36b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e3100000000000000000000000000000000000000000000000000
0000
You can also produce an animated version of thedeformed shape:
71Utility Menu> Plot Ctrls> Animate> Deformed Shape
2Choose Def + undeformed.3OK.
8ffd8ffe000104a46494600010201004800480000
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
080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e31000000000000000000000000000000000000000000000000000000
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
02863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e31000000000000000000000000000000000000000000000000000000
9ffd8ffe000104a46494600010201006000600000
ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001
500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000
8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 47/51
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ffd8ffe000104a46494600010201006000600000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e7472524742205859
5a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4
850202000000000000000000000000000000000000000000000000000000000000000000000000
000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b7074000002040000
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46d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f707972696768742
02863292031393938204865776c6574742d5061
636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000000000000000000000000000000000000000000
0000
2.1.8.3. Step 24: Plot the von Mises equivalent stress.
1Main Menu> General Postproc> Plot Results> Contour
Plot> Nodal Solu
2Choose Stress item to becontoured.3Scroll down and choose von
Mises (SEQV).
4OK.
5ffd8ffe000104a46494600010201004800480000
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c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a000002400000001464
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000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000
00000000000000000000000000000000000000000000
ffd8ffe000104a46494600010201004800480000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000
000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004
8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 48/51
300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630
000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000000000000000000000000000000000000000000
00000
6 ffd8ffe000104a46494600010201004800480000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d534654000000004945432073524742000000000
0000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000
146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e79000064657363000000000000001273524742204945433631393
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ffd8ffe000104a46494600010201006000600000
ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a000
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
00000
You can also produce an animated versionof these results:
71Utility Menu> Plot Ctrls> Animate> Deformed Results
2Choose Stress item to be contoured.3Scroll down and choose von Mises (SEQV).
4OK.
8
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500000003364657363000001840000006c77747
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8/4/2019 Plane Stress Bracket Tut
http://slidepdf.com/reader/full/plane-stress-bracket-tut 49/51
080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e3100000000000000000000001273524
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0000
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46540000000049454320735247420000000000000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000204000000147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646
d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000146d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452
430000043c0000080c625452430000043c0000080c7465787400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e3100000000000000000000000000000000000000000000000000
0000
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ffd8ffe000104a46494600010201006000600000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e7472524742205859
5a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000
000000000000000000f6d6000100000000d32d4850202000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b7074000002040000
00147258595a00000218000000146758595a0000022c000000146258595a0000024000000014646d6e640000025400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f80000001
46d6561730000040c0000002474656368000004300000000c725452430000043c0000080c675452430000043c0000080c625452430000043c0000080c7465787400000000436f707972696768742
02863292031393938204865776c6574742d5061636b61726420436f6d70616e790000646573630
000000000000012735247422049454336313936362d322e31000000000000000000000012735247422049454336313936362d322e310000000000000000000000000000000000000000000000000
00000
2.1.8.4. Step 25: List reaction solution.
ffd8ffe000104a46494600010201006000600000ffe20c58
4943435f50524f46494c4500010100000c484c696e6f0210
00006d6e74725247422058595a2007ce000200090006003
10000616373704d53465400000000494543207352474200
00000000000000000000000000f6d6000100000000d32d4
85020200000000000000000000000000000000000000000
00000000000000000000000000000000000000000000000
00000001163707274000001500000003364657363000001840000006c77747074000001f000000014626b707400000
204000000147258595a00000218000000146758595a0000
022c000000146258595a0000024000000014646d6e64000
0025400000070646d6464000002c4000000887675656400
00034c0000008676696577000003d4000000246c756d690
00003f8000000146d6561730000040c0000002474656368
000004300000000c725452430000043c0000080c6754524
30000043c0000080c625452430000043c0000080c746578
7400000000436f70797269676874202863292031393938204865776c6574742d5061636b61726420436f6d70616e79
0006465736300000000000000127352474220494543363
3936362d322e31000000000000000000000012735247422
049454336313936362d322e31000000000000000000000000000000000000000000000000000000
ffd8ffe000104a46494600010201006000600000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74725247422058595a2007ce00020009000600310000616373704d5346540000000049454320735247420000000000
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
00000
The value of 134.61 is comparable to the total pin load force.
Note
The values shown are representative and may vary from
the values you obtain.
There are many other options available for reviewing
results in the general postprocessor. You’ll see some of
these demonstrated in other tutorials. You have finished
the analysis. Exit the program in the next step.
2.1.8.5. Step 26: Exit the ANSYS program.
When exiting the ANSYS program, you can save the geometry
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and loads portions of the database (default), save geometry,
loads, and solution data (one set of results only), save geometry,
loads, solution data, and postprocessing data (i.e., save
everything), or save nothing. You can save nothing here, but you
should be sure to use one of the other save options if you want to
keep the ANSYS data files.
ffd8ffe000104a46494600010201006000600000ffe20c584943435f50524f46494c4500010100000c484c696e6f021000006d6e74
725247422058595a2007ce00020009000600310000616373704d
5346540000000049454320735247420000000000000000000000
000000f6d6000100000000d32d48502020000000000000000000
0000000000000000000000000000000000000000000000000000
0000000000000000000000001163707274000001500000003364
657363000001840000006c77747074000001f000000014626b70
7400000204000000147258595a00000218000000146758595a00
00022c000000146258595a0000024000000014646d6e64000002
5400000070646d6464000002c400000088767565640000034c0000008676696577000003d4000000246c756d69000003f8000000
146d6561730000040c0000002474656368000004300000000c72
5452430000043c0000080c675452430000043c0000080c62545
430000043c0000080c7465787400000000436f7079726967687
202863292031393938204865776c6574742d5061636b6172642
436f6d70616e790000646573630000000000000012735247422
49454336313936362d322e31000000000000000000000012735
47422049454336313936362d322e31000000000000000000000
00000000000000000000000000000000
Congratulations! You have completed this tutorial.
Even though you have exited the ANSYS program, you can
still view animations using the ANSYS ANIMATE program.
The ANIMATE program runs only on the PC and is extremely
useful for:
z
Viewing ANSYS animations on a PC regardless owhether the files were created on a PC (AVI files) or o
a UNIX workstation (ANIM files).
Converting ANIM files to AVI files.
z z
Sending animations over the web.