Analysis of a Truss

ANSYS TUTORIAL

Analysis of a Truss

Copyright 2001-2002, John R. Baker

In this tutorial, you will model and analyze the truss below in ANSYS. Step-by-step instructions are provided beginning on the following page. This problem was adapted from Problem 6-17 in the textbook, Engineering Mechanics - Statics, Third Edition, by R.C. Hibbeler.

If you run into problems with these instructions, feel free to contact:

John Baker; Phone: 270-534-6342; Email: jbaker@engr.uky.edu

The steps that will be followed are:

Preprocessing:

1. Change Jobname.

2. Define element type. (Link1 element which is a 2-D spar)

3. Define real constants. (Area)

4. Define material properties. (Young's Modulus, EX -- only property required for this analysis)

5. Create nodes at truss joints. (8 total)

6. Create link elements between nodes. (13 total)

Solution:

7. Apply constraints and loads to the model.

8. Solve.

Postprocessing:

9. Plot deformed shape.

10. List reaction forces.

11. List a summary of element solution information, including axial forces and stresses.

12. List the deflections at each node.

13. Exit the ANSYS program.

Notes:

Cross-sectional area of truss members = 3.0E-4 m ; Modulus of Elasticity = 2.07E11 psi; Circled numbers shown are node numbers.

Launching ANSYS:

It is probably best to save your work on a Zip Disk in the computer IOMEGA Zip Drive. On any machine in the computer lab (on the first floor of Crounse Hall), insert a Zip Disk in the drive. Then, simply click on the ANSYS icon on the Windows Desktop. The ANSYS Launcher menu should appear. It is shown at the top of the next page. The only input you will likely need on this menu is specification of the Zip Drive as your "Working Directory". If you don't have a Zip Disk, or if you prefer to work on the computer hard drive instead, then specify any directory (or, "Folder") as your working directory. To browse and find the desired working directory, click on the button with the three dots to the far right on the Launcher Menu on the line that says "Working Directory". Once the working directory is specified, click on "Run" at the bottom of the Launcher Menu.

The ANSYS menus should open up. You will see a Main Menu, illustrated on the following page, and a large black graphics window. You are now ready to begin creating the model and performing the analysis.

ANSYS Launcher Menu:

ANSYS Main Menu:

Note: Most of the required tasks are performed using menu picks from the ANSYS Graphical User Interface, as specified in italics in the step-by-step instructions below. The instructions below also include alternative command line entries that can be ignored if you choose to use menu picks to perform the required tasks. These are provided for your information. You may find that it is sometimes more convenient to enter certain commands directly at the command line.

****IMPORTANT***: AS YOU WORK THROUGH THIS EXERCISE, WITHIN ANSYS, ON THE ANSYS TOOLBAR (UPPER RIGHT), CLICK ON "SAVE_DB" OFTEN!!! THIS TOOLBAR APPEARS AS:

At any point, if you want to resume from the previous time the model was saved, simply click on "RESUM_DB" on this same Toolbar. Any information entered since the last save will be lost, but this is a nice feature in the event that you make an input mistake, and are unsure of how to correct it.

There are a number of ways to model a system and perform an analysis in ANSYS. The steps below present only one method.

Preprocessing:

1. Change jobname: File -> Change Jobname

Enter "truss", and click on "OK".

Alternative Command Line Entry = /filnam, truss

Also, to enter the preprocessor, at the command line, enter: /prep7

2. Define element types: Preprocessor -> Element Type -> Add/Edit/Delete

Click on "Add , highlight "Link", then "2D spar", click on "OK", then "Close". Note that in ANSYS this element is sometimes referred to as "Link1", because it is element type 1 in the ANSYS element library.

Alternative Command Line Entry = et,1,1

3. Define the real constants for the Link1, which are cross-sectional area and initial strain:

Preprocessor -> Real Constants -> Add

Click "OK" for "Type 1 LINK1"

In this problem, there is no initial strain (leave blank), and the area is 3.0E-4. After filling in the area value, click on "OK", then "Close".

Alternative Command Line Entry = r,1,3.0E-4

4. Define Material Properties: Preprocessor -> Material Properties -> -Constant- Isotropic

"OK" for material set number 1, then enter 30E6 for EX, then "OK".

Alternative Command Line Entry = ex,1,2.07E11

5. Create nodes at truss joints: Preprocessor -> -Modeling- Create -> Nodes -> In Active CS

Enter 1 for node number (ANSYS would automatically number nodes if you leave this blank). Enter the location as (X,Y,Z)=(0,0,0). Note that we are entering the locations in meters, with node 1 located at the origin of the global x-y-z Cartesian coordinate system. Leave the entries for rotation angles blank. (Note: For this problem, all nodes will be in the X-Y plane, with Z=0). Click on "Apply". Continue defining nodes 2-8 using the locations based on the sketch of the truss, but after entering the node 8 location, click on "OK" instead of "Apply". So, node 2 is at (X,Y)=(3,0), node 3 is at (X,Y)=(6,0), node 4 is at (X,Y)=(9,0), node 5 is at (X,Y)=(12,0), node 6 is at (X,Y)=(3,3), node 7 is at (X,Y)=(6,3), and node 8 is at (X,Y)=(9,3). The dimensions entered are in inches, and on the node definition menu, for our case, rotation angles are ignored, and for all nodes, Z=0.

Alternative Command Line Entry = n

Alternative Command Line Entry = n,2,3,0,0 (or, simply: n,2,3; then similar command for all other nodes - missing input is interpreted by ANSYS as "zero" in most cases).

As a check to ensure all nodes were entered correctly, list the nodes:

Utility Menu ->List -> Nodes

Alternative Command Line Entry = nlist

If any errors were made in defining the nodes, you can redefine a node by repeating the procedure of step 5. Of course, you don't need to redefine all nodes simply to move one. Just repeat the node creation command for the incorrectly placed node.

Turn on node numbering. Utility Menu -> PlotCtrls -> Numbering. Check "node numbering", then click "OK". The node numbers may already be showing, but this will force the display of node numbers on subsequent plots.

Alternative Command Line Entry = /pnum,node,1

Create link elements between nodes:

Preprocessor -> Create -> Elements ->-Auto Numbered-Thru Nodes

A picking menu appears. Pick node 1, then node 2, and click on "Apply" in the Picking Menu. Continue creating elements using the definitions listed in the table below. After picking the nodes for the last element (element 13), choose "OK" (instead of "Apply") to define the element and close the picking menu.

Element Node I Node J

1 1 2

2 2 3

3 3 4

4 4 5

5 1 6

6 2 6

7 3 6

8 3 7

9 3 8

10 4 8

11 5 8

12 6 7

13 7 8

Alternative Command Line Entry = e

Alternative Command Line Entry = e (and so on for the remaining elements)

Solution:

If entering commands at the command line, to enter the solution processor, type: /solu

Apply constraints and forces on the model:

Solution -> -Loads- Apply -> -Structural- Displacement -> On Nodes

Pick node 5, then click "OK" in the picking menu that has appeared. Choose ALL DOF, and use the default displacement value of zero. Click on "Apply". Pick node 1, then click "OK" in the picking menu. To constrain this node in the Y-direction only, Click on "UY". Make sure to unselect the "ALL DOF" label! If the "ALL DOF" label is highlighted, unselect it by clicking on it. After confirming that only "UY" is highlighted, click "OK".

Alternative Command Line Entry = d,5,all,0

Alternative Command Line Entry = d,1,uy,0

To apply the forces, choose:

Solution -> -Loads- Apply -> -Structural- Force/Moment -> On Nodes

Pick node 2, then "OK" in the picking menu, choose "FY" as the direction of the force, and enter -125 for the force value. Click on "Apply". Pick node 3, click "OK" in the picking menu, and enter -100 for the force value (still in the FY direction). Click on "OK".

Alternative Command Line Entry = f,2,fy,-125

Alternative Command Line Entry = f,3,fy,-100

8. Solve the problem: Solution -> -Solve- Current LS

Click "OK" in the "Solve Current Load Step" Box.

Alternative Command Line Entry = solve

Postprocessing:

If entering commands at the command line, to enter the postprocessor, type: /post1

9. Plot the deformed shape: General Postproc -> Plot Results -> Deformed Shape

You will probably want to choose "Def + undeformed", then "OK".

Alternative Command Line Entry = pldi

10. List reaction forces: General Postproc -> List Results -> Reaction Solution

Click on "All struc forc F", and "OK".

Alternative Command Line Entry = prrf

You might want to print the information in the Listing Box, by clicking, in that box, on "File -> Print". Or else, just write the information down.

11. List a summary, which includes the axial force and stress in each element:

General Postproc -> List Results -> Element Solution -> LineElem results -> Structural ELEM

Click "OK", and a summary for each element is printed, including the node numbers, from which you can identify the corresponding truss member, and also the axial force (MFORX), and the axial stress (SAXL). You may want to either record, or print, this information.

12. List the x and y direction deflections for each node:

General Postproc -> List Results -> Nodal Solution -> DOF Solution -> ALL DOFs

Click "OK". Again, you may want to either record, or print, this information.

Alternative Command Line Entry = prdi

13. Exit ANSYS. Toolbar: Quit ->Save Everything -> OK