Chris Allbee
11-10-2009, 01:34 PM
I'm not terribly familiar with the settings available in solidworks, but if you can make sure that the joints are not pin connections. If you have a node in the middle of a main tube then a pin connection will not provide the appropriate stiffness (think moment continuity across that main tube). Beyond that just make sure your sections are defined properly, again not familiar with solidworks, but most FEA software require a section orientation in addition to the beam axis.
In general an analytical beam simulation will OVER predict the stiffness of the frame.
In order to make sure you have the best comparison double-check your constraints and make sure they match the test condition as best as you can. If you have the capability, look at the mode shapes of the first few modes, torsion and bending at least, and make sure they seem reasonable.
You will always have a relatively large discrepancy when using analytical elements, and if you want more accuracy then you will need to move to using at least 2D shell elements.
If your school doesn't have access to real FEA software I think that Altair provides university licenses for free, or at least they used to. Their Hyperworks suite is pretty powerful and even has a built-in solver that can handle simple static loadings and even optimizations with relative ease.
In any case I recommend getting a proper pre/post-processor and solver package if you are aiming for decent accuracy, as within 5% of actual.
ed_pratt
11-11-2009, 08:57 AM
I wouldn't bother, unless your SolidWorks model is perfect you'll get dodgy results anyway.
For the purposes of using FEA to better optimise your chassis you're as well to start from scratch with an input file - written in notepad/wordpad - and tell ABAQUS where the nodes are and which which elements to use to connect them up.
Here is a VERY simple example. (copy into wordpad and save as a .inp file to run in ABAQUS)
There are some glarringly obvious problems (purposely) with this model, however, it should be enough to get you started.
Best of luck,
Ed
------------------------------------------------
*HEADING
FSAE CHASSIS ANALYSIS
*PREPRINT, ECHO=YES
*RESTART, WRITE
*NODE
1, 0., 0., 0.
2, 0.41, 0., 0.
3, 0.41, 0.41, 0.
4, 0., 0.41, 0.
5, 0., 0., 1.
6, 0.41, 0., 1.
7, 0.41, 0.41, 1.
8, 0., 0.41, 1.
9, 0., 0., 1.7
10, 0.41, 0., 1.7
11, 0.41, 0.41, 1.7
12, 0., 0.41, 1.7
13, 0., 0.45, 1.
14, 0.41, 0.45, 1.
15, 0.15, 0.53, 1.
16, 0.26, 0.53, 1.
17, 0., 0.53, 1.7
18, 0.41, 0.53, 1.7
19, 0.15, 0.9, 1.7
20, 0.26, 0.9, 1.7
21, 0.205, 0.98, 1.7
*ELEMENT, ELSET=TRUSS, TYPE=T3D2
1, 1, 2
2, 2, 3
3, 1, 4
4, 4, 3
5, 2, 6
6, 1, 5
7, 4, 8
8, 3, 7
9, 5, 6
10, 6, 7
11, 5, 8
12, 8, 7
13, 8, 13
14, 7, 14
15, 6, 10
16, 7, 11
17, 8, 12
18, 5, 9
19, 10, 11
20, 11, 12
21, 12, 9
22, 9, 10
23, 13, 15
24, 15, 16
25, 16, 14
26, 14, 7
27, 4, 15
28, 3, 16
29, 12, 17
30, 17, 19
31, 19, 21
32, 21, 20
33, 20, 18
34, 18, 11
35, 1, 3
36, 1, 6
37, 5, 10
38, 2, 7
39, 7, 10
40, 1, 8
41, 8, 9
42, 9, 11
*SOLID SECTION, ELSET=TRUSS, MATERIAL=STEEL
0.00024
*MPC
TIE, 15, 16
*MATERIAL, NAME=STEEL
*ELASTIC
209E9, 0.3
*NSET, NSET=rollbar
11, 12, 17, 18, 19, 20, 21
*BOUNDARY
rollbar, encastre
9, ENCASTRE
10, ENCASTRE
11, ENCASTRE
12, ENCASTRE
*STEP
*STATIC
*CLOAD
3, 2, 2000
4, 2, 2000
*NODE PRINT
U, RF
*EL PRINT
S, E
*END STEP
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