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Shuvom Ghose 
800-424-2255 x1110 
shuvom@capinc.com 
www.capinc.com 
The Summer of Simulation #3: 
5 things you 
should do before 
showing your 
FEA results to 
anyone
is ’s leading 
reseller of SolidWorks CAD and 
tools, and 
Stratasys 3D printers.
Slides prepared by CAPINC Engineer: 
Who makes work 
with your company’s specific 
Shuvom Ghose
© CAPINC 
• There will always be people who 
doubt your FEA results (and FEA 
use in general). 
• Don’t give the doubters any 
more ammunition. 
• Do all you can to solidify your 
FEA results before showing 
them to people.
1. Ask the right question. 
2. Do a sanity check. Any check. 
3. Make sure the mesh doesn’t matter. 
4. Test a second failure condition. 
5. Document your assumptions. 
© CAPINC
Titanium: 
Ti-6AL-4V 
Fixed at 4 corners 
8000 lbs. 
Total upward 
force 
If you were given this aircraft 
bracket to analyze, what would you 
ask of FEA first? 
Many folks might ask: “What is the maximum stress in the 
bracket? Within, say, +/- 10 percent?” 
(Bracket model courtesy of user “optimal_aj” from GrabCAD.com)
Is 
Ti-6AL-4V 
the closest alloy? 
Is Fixed a realistic 
constraint for 
these bolts? 
Is 8000 lbs. 
really the right 
force? What if 
the load is at an 
angle? 
But if you ask about the absolute 
stress, now EVERY aspect of your 
study is called into question: 
Is this mesh fine 
enough for this 
complex geometry?
Worse than that, now you’ll get into 8000 lbs.? 
the “Percentage Game” with your 
doubters. You’ll say: 
“Given all these questions, the max 
stress is probably accurate within 
15%.” 
Fixed? 
Ti-6AL-4V? 
Mesh fine 
enough? 
“15 percent? HA! You’ll need 
accuracy better than +/- 5 percent to 
convince ME!”
Fixed 
Upward force 
But instead of 
maximum stress, what 
if you asked: 
“We’ve got two 
competing bracket 
designs. Which one is 
better?” 
© CAPINC
Then, with just a 1 
minute FEA study, you 
learn that the lower 
bracket is: 
77% Heavier 
16% Worse 
displacement in 
the pull direction 
© CAPINC 
(Same load, mesh settings, 
fixtures, material)
77% Heavier 
16% Worse 
displacement 
And the best part is, all those 
doubts we had with the absolute 
study fall away, since they are 
the same for both relative 
bracket studies! 
This means doubters can’t object 
to the results! 
© CAPINC 
“Um…” 
(Same load, mesh settings, 
fixtures, material)
77% heavier 
16% worse Z disp. 
160% heavier 
50% better Z disp. 
216% heavier 
34% better Z disp.
At CAPINC, we call this the “A vs. B comparison”. Use it to make 
your FEA cycles faster, since EVERY design decision can be boiled 
down to a choice of: “Do we do this? Or this? Or neither?” 
© CAPINC
1. Ask the right question. 
2. Do a sanity check. Any 
check. 
3. Make sure the mesh doesn’t 
matter. 
4. Test a second failure 
condition. 
5. Document your assumptions. 
© CAPINC
Returning to absolute 
numbers, with 8000 lbs. 
upward force on the lugs, the 
maximum reported stress in 
the part is: 
3.6e5 psi. 
© CAPINC 
Is that way too much? Way too 
little? In the ballpark? If we’ve 
never seen a shape like this, how 
can we tell?
Is your max stress 
right next to one of 
your restrained, 
rigidly fixed faces? 
Then the number 
is fake. 
The fixed face distorts the stress around it, since one 
end of those mesh nodes can’t move at all, leading to 
more stress on the element. To get a more accurate 
number, we’d have to change the fixed restraint, or 
model the bolts and plate they’re attached to.
© CAPINC 
Using a Design Insight plot (found 
in all levels of SolidWorks 
Simulation), we can see that the 
back legs carry most of the stress 
when this bracket is pulled upward. 
Blue= loaded
8000 lbs. 
Total upward force 
Stresses ~ 
4e4 psi? 
© CAPINC 
Using an Iso Clipping plot (found in 
all levels of SolidWorks Simulation), 
we can see that the stress in those 
loaded back legs is around 4e4 psi. 
Is that way too much? Not enough? 
How can we tell?
© CAPINC 
And if you look at those back legs and 
squint a little, that back leg is sort of a 
cylinder about 0.5” diameter:
© CAPINC 
8000 lbs. 
So what would happen if we 
took a cylinder of that size 
and put 8000 lbs. of load on 
it?
8000 lbs. upward force 
on test coupon 
Stresses = 4e4 
psi in 0.5” dia 
section 
8000 lbs. Total upward force 
on bracket 
Stresses ~ 
4e4 psi in 
~0.5” dia 
leg 
With results in the same magnitude (e4 psi), we can conclude that our 
initial stress results are… NOT INSANE. That’s all we can tell.
8000 lbs. upward force 
on test coupon 
4e4 psi 
© CAPINC 
“You’re estimating the 
stresses in your part 
with a cylinder under 
tension? 
I can do what with a 
simple hand calculation! 
Why do we need some 
fancy, expensive FEA 
package to accomplish 
that!?! 
Back in my day…”
© CAPINC
On-line Hoop Stress Calculator: 
http://www.engineersedge.com/calculators/hoop-stress. 
htm 
© CAPINC
© CAPINC
• What’s the MOST this number could be? 
• What’s the LEAST? 
• What is the range of your plot’s legend? 
• Are deformations still “Elastic”, i.e. are 
they under 0.2% strain? (Linear solvers 
assume all deformations are elastic.) 
© CAPINC
1. Ask the right question. 
2. Do a sanity check. Any 
check. 
3. Make sure the mesh doesn’t 
matter. 
4. Test a second failure 
condition. 
5. Document your assumptions. 
© CAPINC
31,000 
mesh 
elements 
© CAPINC 
How many mesh 
elements are 
‘enough’? 
126,000 
mesh 
elements
One big mesh element is like one big spring, pretty stiff… 
© CAPINC 
Many mesh elements are like many small springs, 
added all together, they bend more while staying in 
the elastic zone…
© CAPINC 
Tip displace: 
5.14e-8 in 
Tip displace: 
5.27e-8 in
© CAPINC 
Increasing mesh density 
Result 
‘Real’ 
answer 
What ‘should’ happen as 
you increase mesh 
density
© CAPINC 
Mesh elements 
Z displacement, 
(in)
© CAPINC 
Mesh elements 
Z displacement, 
(in) 
Mesh elements
Ask the right question! 
Mesh accuracy doesn’t 
matter if the second A 
vs. B design is heavier 
AND worse in 
displacement! 
© CAPINC 
77% Heavier 
16% Worse Z 
Displacement 
1 minute FEA study
© CAPINC 
Mesh elements 
Your result number
1. Ask the right question. 
2. Do a sanity check. Any 
check. 
3. Make sure the mesh doesn’t 
matter. 
4. Test a second failure 
condition. 
5. Document your assumptions. 
© CAPINC
© CAPINC 
8500 lbs.?
© CAPINC 
5000 in-lbs.
© CAPINC
 Things Breaking 
 Things Bending too much 
 Things Overheating 
 Things Shaking at Nat. Freqs. 
 Long, Slender Things Buckling 
 Fatigue Failure 
© CAPINC 
Break 
Bend 
Burn 
Buzz 
Buckle 
Fat 
BBBBBFat! 
We checked for:
© CAPINC
© CAPINC
SolidWorks Simulation Professional: 
Break and Bend Buzz 
© CAPINC 
Burn 
Fatigue Optimize 
Buckle
1. Ask the right question. 
2. Do a sanity check. Any 
check. 
3. Make sure the mesh doesn’t 
matter. 
4. Test a second failure 
condition. 
5. Document your assumptions. 
© CAPINC 
BBBBBFat!
Restraints 
Material Properties 
© CAPINC 
Loads 
Mesh 
Contact Conditions 
Geometry 
Simplification
Restraints 
Material Properties 
© CAPINC 
Loads 
Mesh 
Contact Conditions 
Geometry 
Simplification
© CAPINC 
• Restraints 
• Mesh • Geometry 
Simplification 
• Contact Conditions 
• Loads 
• Material Properties 
BIGGER 
assumptions 
Smaller 
assumptions
Appendix F: Assumptions 
• Bracket variant 142A was restrained with fixed faces 
© CAPINC 
at each of its bolt corners.
Section 2: Assumptions (BEFORE results!) 
• Bracket variant 142A was restrained with fixed faces 
(green) at each of its bolt corners: 
© CAPINC
Section 2: Assumptions 
• Bracket variant 142A was restrained with bolt faces only allowed 
rotational motion (green cylinders) and bottom faces only allowed 
sliding motion (orange planes): 
© CAPINC
1. Ask the right question. 
2. Do a sanity check. Any 
check. 
3. Make sure the mesh doesn’t 
matter. 
4. Test a second failure 
condition. 
5. Document your assumptions. 
© CAPINC 
BBBBBFat!
© CAPINC 
• 3 rules to do material 
selection right 
• 10 designs by hand, 
100 by FEA 
• 5 things to do before 
anyone sees your FEA 
results 
http://www.capinc.com/events/webinars/recorded-webinars
If you want cutting edge or 
, contact 
(salesinfo@capinc.com) 
If you want more info on the FEA 
concepts presented, contact: 
(shuvom@capinc.com)

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CAPINC Summer of Simulation Part 3: The 5 Things to do Before Showing Anyone your FEA Results

  • 1. Shuvom Ghose 800-424-2255 x1110 shuvom@capinc.com www.capinc.com The Summer of Simulation #3: 5 things you should do before showing your FEA results to anyone
  • 2. is ’s leading reseller of SolidWorks CAD and tools, and Stratasys 3D printers.
  • 3. Slides prepared by CAPINC Engineer: Who makes work with your company’s specific Shuvom Ghose
  • 4. © CAPINC • There will always be people who doubt your FEA results (and FEA use in general). • Don’t give the doubters any more ammunition. • Do all you can to solidify your FEA results before showing them to people.
  • 5. 1. Ask the right question. 2. Do a sanity check. Any check. 3. Make sure the mesh doesn’t matter. 4. Test a second failure condition. 5. Document your assumptions. © CAPINC
  • 6. Titanium: Ti-6AL-4V Fixed at 4 corners 8000 lbs. Total upward force If you were given this aircraft bracket to analyze, what would you ask of FEA first? Many folks might ask: “What is the maximum stress in the bracket? Within, say, +/- 10 percent?” (Bracket model courtesy of user “optimal_aj” from GrabCAD.com)
  • 7. Is Ti-6AL-4V the closest alloy? Is Fixed a realistic constraint for these bolts? Is 8000 lbs. really the right force? What if the load is at an angle? But if you ask about the absolute stress, now EVERY aspect of your study is called into question: Is this mesh fine enough for this complex geometry?
  • 8. Worse than that, now you’ll get into 8000 lbs.? the “Percentage Game” with your doubters. You’ll say: “Given all these questions, the max stress is probably accurate within 15%.” Fixed? Ti-6AL-4V? Mesh fine enough? “15 percent? HA! You’ll need accuracy better than +/- 5 percent to convince ME!”
  • 9. Fixed Upward force But instead of maximum stress, what if you asked: “We’ve got two competing bracket designs. Which one is better?” © CAPINC
  • 10. Then, with just a 1 minute FEA study, you learn that the lower bracket is: 77% Heavier 16% Worse displacement in the pull direction © CAPINC (Same load, mesh settings, fixtures, material)
  • 11. 77% Heavier 16% Worse displacement And the best part is, all those doubts we had with the absolute study fall away, since they are the same for both relative bracket studies! This means doubters can’t object to the results! © CAPINC “Um…” (Same load, mesh settings, fixtures, material)
  • 12. 77% heavier 16% worse Z disp. 160% heavier 50% better Z disp. 216% heavier 34% better Z disp.
  • 13. At CAPINC, we call this the “A vs. B comparison”. Use it to make your FEA cycles faster, since EVERY design decision can be boiled down to a choice of: “Do we do this? Or this? Or neither?” © CAPINC
  • 14. 1. Ask the right question. 2. Do a sanity check. Any check. 3. Make sure the mesh doesn’t matter. 4. Test a second failure condition. 5. Document your assumptions. © CAPINC
  • 15. Returning to absolute numbers, with 8000 lbs. upward force on the lugs, the maximum reported stress in the part is: 3.6e5 psi. © CAPINC Is that way too much? Way too little? In the ballpark? If we’ve never seen a shape like this, how can we tell?
  • 16. Is your max stress right next to one of your restrained, rigidly fixed faces? Then the number is fake. The fixed face distorts the stress around it, since one end of those mesh nodes can’t move at all, leading to more stress on the element. To get a more accurate number, we’d have to change the fixed restraint, or model the bolts and plate they’re attached to.
  • 17. © CAPINC Using a Design Insight plot (found in all levels of SolidWorks Simulation), we can see that the back legs carry most of the stress when this bracket is pulled upward. Blue= loaded
  • 18. 8000 lbs. Total upward force Stresses ~ 4e4 psi? © CAPINC Using an Iso Clipping plot (found in all levels of SolidWorks Simulation), we can see that the stress in those loaded back legs is around 4e4 psi. Is that way too much? Not enough? How can we tell?
  • 19. © CAPINC And if you look at those back legs and squint a little, that back leg is sort of a cylinder about 0.5” diameter:
  • 20. © CAPINC 8000 lbs. So what would happen if we took a cylinder of that size and put 8000 lbs. of load on it?
  • 21. 8000 lbs. upward force on test coupon Stresses = 4e4 psi in 0.5” dia section 8000 lbs. Total upward force on bracket Stresses ~ 4e4 psi in ~0.5” dia leg With results in the same magnitude (e4 psi), we can conclude that our initial stress results are… NOT INSANE. That’s all we can tell.
  • 22. 8000 lbs. upward force on test coupon 4e4 psi © CAPINC “You’re estimating the stresses in your part with a cylinder under tension? I can do what with a simple hand calculation! Why do we need some fancy, expensive FEA package to accomplish that!?! Back in my day…”
  • 24. On-line Hoop Stress Calculator: http://www.engineersedge.com/calculators/hoop-stress. htm © CAPINC
  • 26. • What’s the MOST this number could be? • What’s the LEAST? • What is the range of your plot’s legend? • Are deformations still “Elastic”, i.e. are they under 0.2% strain? (Linear solvers assume all deformations are elastic.) © CAPINC
  • 27. 1. Ask the right question. 2. Do a sanity check. Any check. 3. Make sure the mesh doesn’t matter. 4. Test a second failure condition. 5. Document your assumptions. © CAPINC
  • 28. 31,000 mesh elements © CAPINC How many mesh elements are ‘enough’? 126,000 mesh elements
  • 29. One big mesh element is like one big spring, pretty stiff… © CAPINC Many mesh elements are like many small springs, added all together, they bend more while staying in the elastic zone…
  • 30. © CAPINC Tip displace: 5.14e-8 in Tip displace: 5.27e-8 in
  • 31. © CAPINC Increasing mesh density Result ‘Real’ answer What ‘should’ happen as you increase mesh density
  • 32. © CAPINC Mesh elements Z displacement, (in)
  • 33. © CAPINC Mesh elements Z displacement, (in) Mesh elements
  • 34. Ask the right question! Mesh accuracy doesn’t matter if the second A vs. B design is heavier AND worse in displacement! © CAPINC 77% Heavier 16% Worse Z Displacement 1 minute FEA study
  • 35. © CAPINC Mesh elements Your result number
  • 36. 1. Ask the right question. 2. Do a sanity check. Any check. 3. Make sure the mesh doesn’t matter. 4. Test a second failure condition. 5. Document your assumptions. © CAPINC
  • 37. © CAPINC 8500 lbs.?
  • 38. © CAPINC 5000 in-lbs.
  • 40.  Things Breaking  Things Bending too much  Things Overheating  Things Shaking at Nat. Freqs.  Long, Slender Things Buckling  Fatigue Failure © CAPINC Break Bend Burn Buzz Buckle Fat BBBBBFat! We checked for:
  • 43. SolidWorks Simulation Professional: Break and Bend Buzz © CAPINC Burn Fatigue Optimize Buckle
  • 44. 1. Ask the right question. 2. Do a sanity check. Any check. 3. Make sure the mesh doesn’t matter. 4. Test a second failure condition. 5. Document your assumptions. © CAPINC BBBBBFat!
  • 45. Restraints Material Properties © CAPINC Loads Mesh Contact Conditions Geometry Simplification
  • 46. Restraints Material Properties © CAPINC Loads Mesh Contact Conditions Geometry Simplification
  • 47. © CAPINC • Restraints • Mesh • Geometry Simplification • Contact Conditions • Loads • Material Properties BIGGER assumptions Smaller assumptions
  • 48. Appendix F: Assumptions • Bracket variant 142A was restrained with fixed faces © CAPINC at each of its bolt corners.
  • 49. Section 2: Assumptions (BEFORE results!) • Bracket variant 142A was restrained with fixed faces (green) at each of its bolt corners: © CAPINC
  • 50. Section 2: Assumptions • Bracket variant 142A was restrained with bolt faces only allowed rotational motion (green cylinders) and bottom faces only allowed sliding motion (orange planes): © CAPINC
  • 51. 1. Ask the right question. 2. Do a sanity check. Any check. 3. Make sure the mesh doesn’t matter. 4. Test a second failure condition. 5. Document your assumptions. © CAPINC BBBBBFat!
  • 52. © CAPINC • 3 rules to do material selection right • 10 designs by hand, 100 by FEA • 5 things to do before anyone sees your FEA results http://www.capinc.com/events/webinars/recorded-webinars
  • 53. If you want cutting edge or , contact (salesinfo@capinc.com) If you want more info on the FEA concepts presented, contact: (shuvom@capinc.com)

Editor's Notes

  1. In fact, these are all conditions of the original spec. We can do better.
  2. Tell V-22 story here