BuckeyeMike55
05-21-2007, 12:32 PM
I wouldn't use ANY FEA package aside from ANSYS Classical for this analysis (or some equivalent program). Having taken a course on FEM using ANSYS classic, there is no really good way to approach analysis of a tube frame chassis other than ANSYS classic, and I give you this reason:
FEA programs with a beautiful GUI lack the ability to apply a load at a nodal point (where your tubes meet together). Don't quote me on that, but it has been my experience that it is rather difficult to correctly load your chassis using 'pretty' GUI FEA programs, such as ANSYS workbench and COSMOS, because they only allow you to select loads at the following places (in the case of a round-tubular joint):
1) Along the Cross-sectional face (great, if you're doing a tensile test of a beam not at a joint)
2) The outer or inner diameter of the tube at the cross section (unrealistic loading)
3) Along the ENTIRE face of the tube (I don't think i need to explain the errors with this approach)
I taught our chassis leader this year how to model through using BEAM 188 ELEMENT, keypoints, lines meshes, and applied COMMON BEAM SECTIONS and after having used ANSYS classic for analysis of a tube chassis he wouldnt use anything else to approach chassis design of a tube-frame car. ANSYS can be a bit frustrating to new users, as you may know any error and you have to restart the program over. However, if you didn't know the .txt file method this is where ANSYS becomes less cumbersome.
Whenever I analyze anything using ANSYS Classic 10.0, I always save my steps by going to file >> write DB log file >> (select the dropbox) >> write essential commands only. Locate the file, open it with notepad and you can then copy and paste that into the command window and it will repeat every step you made. This also works with IGES / .SAT imported analysis, as long as you have the directory location of the file correct at the top of the text file.
If this is all old news to you, great. I would highly recommend approaching your analysis using the method i described. I've included a file of a square box with displacements and loads so you will have a better idea of what im talking about.
>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>
KEYW,PR_STRUC,1 !Selecting structural menu (preferences)
KEYW,PR_THERM,0
KEYW,PR_FLUID,0
KEYW,PR_ELMAG,0
KEYW,MAGNOD,0
KEYW,MAGEDG,0
KEYW,MAGHFE,0
KEYW,MAGELC,0
KEYW,PR_MULTI,0
KEYW,PR_CFD,0
/prep7
ET,1,BEAM188 !Beam Type
MPTEMP,,,,,,,, !Material Property
MPTEMP,1,0
MPDATA,EX,1,,30e6 !Modulus of Elasticity (30e6)
MPDATA,PRXY,1,,.29 !Poisson's Ratio (.29)
SECTYPE, 1, BEAM, CTUBE, , 0 !Beam Section Type (This case, round tube with .9" ID, 1.0" OD, 10 divisions (finer mesh))
SECOFFSET, CENT
SECDATA,.9,1,10,0,0,0,0,0,0,0
k,1,0 !Entering keypoints for lines
k,2,10,0,0
k,3,0,0,10
k,4,10,0,10
k,5,0,10,0
k,6,10,10,0
k,7,10,10,10
k,8,0,10,10
l,1,2 !Now connect the dots! (like you did in kindergarten)
l,2,4
l,4,3
l,3,1
l,1,5
l,5,6
l,6,7
l,7,8
l,5,8
l,7,4
l,6,2
l,8,3
FLST,5,12,4,ORDE,2 !Meshing the lines with the circular cross section
FITEM,5,1
FITEM,5,-12
CM,_Y,LINE
LSEL, , , ,P51X
CM,_Y1,LINE
CMSEL,,_Y
LESIZE,_Y1,.2, , , , , , ,1 !Mesh every .20 inches
FLST,2,12,4,ORDE,2
FITEM,2,1
FITEM,2,-12
LMESH,P51X !End Mesh
/eshape,1 !View graphic representation, NOTE: Joints shown are purely graphical (for stress plots), and the actual representation of each joint is a node with lines connecting.
d,1,all !Fixing the "left" wall
d,351,all
d,201,all
d,102,all
f,463,fy,1200 !Applying load along tube, near midsection-top, in the x and y direction
f,463,fx,3000
/solu
solve
/post1 !Postprocessing
PRRSOL !List all Nodal Reactions
PLESOL, S,EQV, 0,1.0 !Von Mises Stress Plot
>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>
NODAL REACTIONS:
NODE FX FY FZ MX MY MZ
1 -212.95 -170.84 -86.227 268.47 453.22 -972.43
102 -1088.1 -688.36 -86.227 268.47 453.22 -3442.5
201 190.91 -111.01 86.227 278.52 -563.42 -803.83
351 -1889.9 -229.79 86.227 278.52 -563.42 -2171.2
http://img518.imageshack.us/my.php?image=file002ho5.jpg
As far as importing your chassis into ANSYS... you will most likely have to model it in Solidworks, SolidEdge, Catia, or whatever CAD program you have and then take all of the points relative to an origin and enter them as keypoints. Then connect the dots (This can be a bit tedious, but it can all be done in 1-2 hours, and after it's done, modifying the points is relatively easy).
If anyone wants a more detailed tutorial, I would be happy to help. Some of the commands are fairly self explanatory, but I did skip a lot of the graphical stuff here.
Coombesy
05-21-2007, 03:04 PM
Just a bit on shell vs beam and a little bit on workbench, I can't comment on cosmos as I haven't used it.
I believe anysys workbench to be better for the vast majority of simulation of solid models, particularly because of the loading methods. It is much easier to apply grouped, more realistic loads that in anysys classic. While you can't apply loads to individual nodes in workbench, at least I don't think you can easily; this is not reprehensive of loads in a solid model based structure. Off the top of my head, you can load bodies, faces/surface, lines and vertices, which I tend to think is sufficient for most models.
For doing beam and truss analysis I use classic, for all the above reasons.
In the reference to beams vs shells, both work and beams are much quicker to solve, though slower to setup initially. I prefer using the solid model with a shell mesh, and being able to rip it from cad, to FEA, analyse make any changes in cad, whip it back to FEA, and damn near just hit solve again. (which is partially easy with workbench and the proE interface). Solve time hasn't proved an issue so far, with a good mesh on the front of the chassis, it was less than 5 minutes (probably 2-3, I can't really remember), which is fine for what I was looking for.
Truth be told I am using Ansys Classic at the moment for the chassis, because I am better able to control the mesh from there and manipulate the model. The final analysis of the final chassis will probably be done in workbench.
None the less, I believe both methods work fine, and in this case it's pretty much a matter of preference.
BuckeyeMike55
05-21-2007, 04:23 PM
I agree Coomesy. Because of the solidworks plugin for Workbench, and the ease at which you can change parts and update / start a new analysis within a workbench 'project' file, I love workbench for solid model analysis (I.E. drivetrain components, mounts, brackets, etc). I used COSMOS a few years back, but it is much less user friendly when it comes to running several different scenarios for the same part (i.e. different iterations and saving each analysis of the different iterations within the same file). Workbench is extremely easy to use, you never have to overwrite old analysis / iterations, and it has a relatively small learning curve. As I was told by a TA that worked in industry for a while: First you learn Workbench, then you learn Classic ANSYS, then you move on to LS-DYNA. I've never seen LS-DYNA and the university is too cheap to get it, but it appears to be a high-end dynamic solver.
Anyways, don't mean to get off track. I'm curious, however, to see how you are going to get better results with workbench than ANSYS Classic on your final chassis. How do you plan to approach it in workbench (citing the flaws I pointed out above with Workbench and similar programs)? Univ. of Cincinatti helped in pointing me in the right direction of Chassis design (with beam elements), and from their torsional rigidity tests they had nearly spot on data in comparison with their ANSYS classic FEA models. Someone from Cincinatti correct me if I'm wrong...
Coombesy
05-21-2007, 05:17 PM
The reasoning is a bit rounds about's but here it is:
We started with our chassis model, and instead of making pipes with a wall thickness, they were left as solids.
This was done specifically so we can send it to ansys, and shell mesh all surfaces, with a set thickness, and quickly look at the overall layout of the chassis.
For these simulations accuracy was not a big issue, it was used for comparative sizing and load pathing. The only reason I used classic was because I knew I could mesh the entire external surface as a shell easily.
Now the that the layout for the chassis is locked in, I plan to use workbench, with quicker loading, ease of adding loading situations "environments". The plan is to use workbench's mid plane extraction tool, and put the correct wall thicknesses in. The solver isn't any more accurate, but the model is.
I haven't validated this method, but it should not be far off. I am very interested in the fact that the beam method you talked about has been validated and accurate.
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