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Leverage reinforced plastics
durability prediction, from
calibration to post-processing
Webinar, 18th September 2019
DSM load bracket fatigue
demonstrator
Pierre Savoyat
Digimat Product Manager
pierre.savoyat@e-xstream.com
Lucien Douven
Research Scientist / Design Engineer
lucien.douven@dsm.com
Confidential2
We are about to release Digimat 2019.1
Confidential3
Witness integrative approach results
targeting structural application
DSM load bracket fatigue
demonstrator
Confidential4
Testing and calibration are challenging,
predictions are much too conservative
Confidential5
Rely on accurate fatigue failure indicator
and easily interpret FEA simulation results
to compute part lifetime
Confidential6
Use Digimat to reach
accurate SFRP fatigue
lifetime predictions
Dedicated environment for
fatigue failure indicator calibration
Dedicated environment for
fatigue lifetime computation
Partner to push limits
Confidential7
e-Xstream engineering is the right partner
to push SFRP fatigue prediction limits
Confidential8
DSM Engineering Plastics
One of the key material suppliers in automotive and electronics
You can find DSM materials in 87% of all cars
Confidential9
Goal : Implement DSM framework in e-Xstream’s Digimat tools
• Enable more accurate part fatigue lifetime predictions
• Improve efficiency and accuracy to calibrate
and validate material cards for high cycle fatigue
(Digimat-MF, Digimat-MX)
• Enable DSM customers by providing an efficient workflow
for part fatigue lifetime evaluation
(Digimat-RP)
So how about the prediction results ?
DSM / e-Xstream collaboration
Improving SFRP fatigue lifetime prediction
Confidential10
Framework CAE fatigue prediction
Flow simulation
Fatigue data Digimat material model Part prediction
Stress concentration
correction
R-value dependence
Anisotropy
Microstructure
Glass fiber orientation
Notch sensitivity
A full overview will be presented at the Digimat User’s Meeting, October 2019
This webinar
Confidential11
Microstructure comparison
Over the path at this location (near failure location), the measured fibre
orientation and predicted orientation (Moldflow V2019) correspond well.
Milled and CT-
scanned domain
Failure
location
Fiber orientation at failure location is predicted well
Confidential12
Part level – Experimental data
0.5
0.1
-0.5
-1
-2𝑅 𝐹 =
𝐹 𝑚𝑖𝑛
𝐹𝑚𝑎𝑥
PA66 GF50, DAM, 23°C
Load bracket test data
Nf,
Confidential13
Part level – Local stress ratio
PA66 GF50, DAM, 23°C
F = -1500 N
F = 1500 N
𝜎 𝑚𝑖𝑛 = −34.3 𝑀𝑃𝑎
𝑅 =
𝐹 𝑚𝑖𝑛
𝐹𝑚𝑎𝑥
𝑡
𝐹 < 0
𝐹 > 0
𝐹
𝜎 𝑚𝑎𝑥 = 94.3 𝑀𝑃𝑎
𝑅 𝜎 ≠ −1
Confidential14
Part level – Local stress ratio
PA66 GF50, DAM, 23°C
𝑅 =
𝐹 𝑚𝑖𝑛
𝐹𝑚𝑎𝑥
𝑡
𝐹 < 0
𝐹 > 0
𝐹
Local stress ratio
The local stress ratio is not equal to the applied load ratio.
The local stress ratio also depends on the magnitude of the load
One needs to correct for the local stress ratio to enable accurate liefetime predictions!
𝑅 = −1
𝑅 = −2
𝑅 = −0.5
𝑅 = 0.1
𝑅 = 0.5
failure location 1
𝑅 ≥ −1
failure location 2
𝑅 < −1
Confidential15
Part level – Local stress ratio
PA66 GF50, DAM, 23°C
anisotropy x R-value x stress concentration x GF prediction
(ans o3ro x -va3 e x stre ss co5centrtion x G?ic =45 x ?)
x10
overestimation
x3
/3 /10
• Failure location captured
• Predictions of complex parts
with accuracy of factor 5-30x
for most R-values.
• R-value dependence
accurately captured
safe
Load bracket
Confidential16
We keep pushing now accounting for local plasticity
Stress
Strain
න 𝜀𝑖𝑗
𝑒
𝑑𝜎𝑖𝑗
𝑒
= න 𝜀𝑖𝑗
𝑒𝑝
𝑑𝜎𝑖𝑗
𝑒𝑝
3D extension of ESED rule
Glinka correction
Elastic
Elastoplastic
• Maintained CPU time
Perform the same elastic simulation
• Enriched inputs for lifetime computation
Estimate plastic stress field
Compute new local R
× 𝐾𝑓
Fatigue data notched specimensFEA results
0°, 0.25mm, R=-1
DSM communication at SPE ACCE 2019
Confidential17
overestimation
Load bracket
safe
x10
x3
/3
/10
Plasticity and stress gradient correction allow
to reach targeted results at part level.
• Failure location captured
• Predictions of complex parts
within 1 decade.
• R-value dependence
accurately captured
Part level – Plasticity correction results
PA66 GF50, DAM, 23°C
Confidential18
overestimation
fine mesh (0.1mm)
coarse (0.75mm)
intermediate (0.5mm)
Load bracket
safe
x10
x3
/3
/10
Plasticity and stress gradient correction allow
to reach targeted results at part level.
• Failure location captured
• Predictions of complex parts
within 1 decade.
• R-value dependence
accurately captured
• Robust to mesh size
Part level – Mesh size robustness
PA66 GF50, DAM, 23°C
Confidential19
Digimat-MX: DSM cards for high cycle fatigue prediction
PA66 GF50
PPA GF50
Two material cards available on request to perform structural analyses
Next: Confirm good results on more applications, are you interested?
DSM / e-Xstream collaboration
Improving SFRP fatigue lifetime prediction
Confidential20
Digimat-MX provides the right environment
for fatigue failure indicator calibration
Confidential21
Similar approach to static failure of SFRP
Failure criteria applies at pseudo grain level
Confidential22
Similar approach to static failure of SFRP
Confidential23
Digimat-MX provides a dedicated calibration environment
Failure trigger
Lifetime target
Parameters
Localization factors
Parameter dependencies
Load ratio
Confidential24
Digimat-MX provides the right environment
for fatigue failure indicator calibration
Confidential25
Digimat-RP provides the right environment
for fatigue lifetime computation
Confidential26
Numerical simulations require extreme care to predict part fatigue lifetime
Elastic
Stress saturation
Stress relaxation
• Elastic material model
• No stress saturation (plasticity)
• No stress relaxation (viscous effects)
Stress
Strain
• Geometric simplification drawbacks
• Faceting
• Non convergence of local extrema
Notched coupon
stress field under
tensile load
Confidential27
Force
Time
𝑰𝒏𝒄.
Constant R
for all elements
Force
Time
𝑰𝒏𝒄. 𝒎𝒊𝒏 and 𝑰𝒏𝒄. 𝒎𝒂𝒙
Spatially varying R
with result assembly
Several workflows allowing a time-accuracy trade off
𝜎 𝑎 and 𝑹 𝝈
𝜎 𝑚𝑖𝑛
𝜎 𝑚𝑎𝑥
𝜎 𝑎 and 𝑹 𝝈
𝜎 𝑚𝑖𝑛
𝜎 𝑚𝑎𝑥
𝜎 𝑎 and 𝑹 𝝈
Force
Time
𝑰𝒏𝒄. 𝒊𝒏𝒊𝒕. and 𝑰𝒏𝒄. 𝒆𝒏𝒅
Spatially varying R
with full cycle
Early design Loading screening Design validation
MarcAvailable for :
Confidential28
Numerous lifetime corrections to account for stress concentration are available
Stress gradient
Interpolation
Correct stress field and
re-compute lifetime
II
I
L
𝝈 𝒆𝒇𝒇. = 𝝈 𝒂𝒕 𝑳
No correction
Same results as FEA
simulation based on
stress field
Lifetime averaging
Average lifetime
predictions in log domain
over a given volume
Stress averaging
Average stress over a
given volume and
re-compute lifetime
Stress gradient
Linear averaging
I
II2L
𝝈 𝒆𝒇𝒇. =
𝟏
𝟐𝑳
න
𝟐𝑳
𝝈𝒅𝒙
Correct stress field and
re-compute lifetime
Stress gradient
Tangent
I
II
𝝈 𝒆𝒇𝒇. =
𝝈 𝒎𝒂𝒙
𝟏 +
𝑳
𝝈 𝒎𝒂𝒙
𝒅𝝈
𝒅𝒙
Correct stress field and
re-compute lifetime
Confidential29
Digimat-RP provides the right environment
for fatigue lifetime computation
Confidential30
Use Digimat to reach
accurate SFRP fatigue
lifetime predictions
Dedicated environment for
fatigue failure indicator calibration
Dedicated environment for
fatigue lifetime computation
Partner to push limits
Confidential31
Benefit from material supplier calibrations
• They already feed Digimat-MX database heavily : +27 fatigue material cards in Digimat 2019.1
Confidential32
Next steps
• What’s new ? → Look at Digimat 2019.1 release webinar
• Interested ? → Look at our case study and come to us to learn more
• Yet customer ? → Benefit from our capabilities and from material cards present in Digimat-MX
• Looking for guidance ? → Benefit from our expertise in testing, calibration and simulation
Leverage reinforced plastics
durability prediction, from
calibration to post-processing
Webinar, 18th September 2019
DSM load bracket fatigue
demonstrator
Thank you!
Q&A
Pierre Savoyat
Digimat Product Manager
pierre.savoyat@e-xstream.com
Lucien Douven
Research Scientist / Design Engineer
lucien.douven@dsm.com

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Leverage reinforced plastics durability prediction, from calibration to post-processing

  • 1. Leverage reinforced plastics durability prediction, from calibration to post-processing Webinar, 18th September 2019 DSM load bracket fatigue demonstrator Pierre Savoyat Digimat Product Manager pierre.savoyat@e-xstream.com Lucien Douven Research Scientist / Design Engineer lucien.douven@dsm.com
  • 2. Confidential2 We are about to release Digimat 2019.1
  • 3. Confidential3 Witness integrative approach results targeting structural application DSM load bracket fatigue demonstrator
  • 4. Confidential4 Testing and calibration are challenging, predictions are much too conservative
  • 5. Confidential5 Rely on accurate fatigue failure indicator and easily interpret FEA simulation results to compute part lifetime
  • 6. Confidential6 Use Digimat to reach accurate SFRP fatigue lifetime predictions Dedicated environment for fatigue failure indicator calibration Dedicated environment for fatigue lifetime computation Partner to push limits
  • 7. Confidential7 e-Xstream engineering is the right partner to push SFRP fatigue prediction limits
  • 8. Confidential8 DSM Engineering Plastics One of the key material suppliers in automotive and electronics You can find DSM materials in 87% of all cars
  • 9. Confidential9 Goal : Implement DSM framework in e-Xstream’s Digimat tools • Enable more accurate part fatigue lifetime predictions • Improve efficiency and accuracy to calibrate and validate material cards for high cycle fatigue (Digimat-MF, Digimat-MX) • Enable DSM customers by providing an efficient workflow for part fatigue lifetime evaluation (Digimat-RP) So how about the prediction results ? DSM / e-Xstream collaboration Improving SFRP fatigue lifetime prediction
  • 10. Confidential10 Framework CAE fatigue prediction Flow simulation Fatigue data Digimat material model Part prediction Stress concentration correction R-value dependence Anisotropy Microstructure Glass fiber orientation Notch sensitivity A full overview will be presented at the Digimat User’s Meeting, October 2019 This webinar
  • 11. Confidential11 Microstructure comparison Over the path at this location (near failure location), the measured fibre orientation and predicted orientation (Moldflow V2019) correspond well. Milled and CT- scanned domain Failure location Fiber orientation at failure location is predicted well
  • 12. Confidential12 Part level – Experimental data 0.5 0.1 -0.5 -1 -2𝑅 𝐹 = 𝐹 𝑚𝑖𝑛 𝐹𝑚𝑎𝑥 PA66 GF50, DAM, 23°C Load bracket test data Nf,
  • 13. Confidential13 Part level – Local stress ratio PA66 GF50, DAM, 23°C F = -1500 N F = 1500 N 𝜎 𝑚𝑖𝑛 = −34.3 𝑀𝑃𝑎 𝑅 = 𝐹 𝑚𝑖𝑛 𝐹𝑚𝑎𝑥 𝑡 𝐹 < 0 𝐹 > 0 𝐹 𝜎 𝑚𝑎𝑥 = 94.3 𝑀𝑃𝑎 𝑅 𝜎 ≠ −1
  • 14. Confidential14 Part level – Local stress ratio PA66 GF50, DAM, 23°C 𝑅 = 𝐹 𝑚𝑖𝑛 𝐹𝑚𝑎𝑥 𝑡 𝐹 < 0 𝐹 > 0 𝐹 Local stress ratio The local stress ratio is not equal to the applied load ratio. The local stress ratio also depends on the magnitude of the load One needs to correct for the local stress ratio to enable accurate liefetime predictions! 𝑅 = −1 𝑅 = −2 𝑅 = −0.5 𝑅 = 0.1 𝑅 = 0.5 failure location 1 𝑅 ≥ −1 failure location 2 𝑅 < −1
  • 15. Confidential15 Part level – Local stress ratio PA66 GF50, DAM, 23°C anisotropy x R-value x stress concentration x GF prediction (ans o3ro x -va3 e x stre ss co5centrtion x G?ic =45 x ?) x10 overestimation x3 /3 /10 • Failure location captured • Predictions of complex parts with accuracy of factor 5-30x for most R-values. • R-value dependence accurately captured safe Load bracket
  • 16. Confidential16 We keep pushing now accounting for local plasticity Stress Strain න 𝜀𝑖𝑗 𝑒 𝑑𝜎𝑖𝑗 𝑒 = න 𝜀𝑖𝑗 𝑒𝑝 𝑑𝜎𝑖𝑗 𝑒𝑝 3D extension of ESED rule Glinka correction Elastic Elastoplastic • Maintained CPU time Perform the same elastic simulation • Enriched inputs for lifetime computation Estimate plastic stress field Compute new local R × 𝐾𝑓 Fatigue data notched specimensFEA results 0°, 0.25mm, R=-1 DSM communication at SPE ACCE 2019
  • 17. Confidential17 overestimation Load bracket safe x10 x3 /3 /10 Plasticity and stress gradient correction allow to reach targeted results at part level. • Failure location captured • Predictions of complex parts within 1 decade. • R-value dependence accurately captured Part level – Plasticity correction results PA66 GF50, DAM, 23°C
  • 18. Confidential18 overestimation fine mesh (0.1mm) coarse (0.75mm) intermediate (0.5mm) Load bracket safe x10 x3 /3 /10 Plasticity and stress gradient correction allow to reach targeted results at part level. • Failure location captured • Predictions of complex parts within 1 decade. • R-value dependence accurately captured • Robust to mesh size Part level – Mesh size robustness PA66 GF50, DAM, 23°C
  • 19. Confidential19 Digimat-MX: DSM cards for high cycle fatigue prediction PA66 GF50 PPA GF50 Two material cards available on request to perform structural analyses Next: Confirm good results on more applications, are you interested? DSM / e-Xstream collaboration Improving SFRP fatigue lifetime prediction
  • 20. Confidential20 Digimat-MX provides the right environment for fatigue failure indicator calibration
  • 21. Confidential21 Similar approach to static failure of SFRP Failure criteria applies at pseudo grain level
  • 22. Confidential22 Similar approach to static failure of SFRP
  • 23. Confidential23 Digimat-MX provides a dedicated calibration environment Failure trigger Lifetime target Parameters Localization factors Parameter dependencies Load ratio
  • 24. Confidential24 Digimat-MX provides the right environment for fatigue failure indicator calibration
  • 25. Confidential25 Digimat-RP provides the right environment for fatigue lifetime computation
  • 26. Confidential26 Numerical simulations require extreme care to predict part fatigue lifetime Elastic Stress saturation Stress relaxation • Elastic material model • No stress saturation (plasticity) • No stress relaxation (viscous effects) Stress Strain • Geometric simplification drawbacks • Faceting • Non convergence of local extrema Notched coupon stress field under tensile load
  • 27. Confidential27 Force Time 𝑰𝒏𝒄. Constant R for all elements Force Time 𝑰𝒏𝒄. 𝒎𝒊𝒏 and 𝑰𝒏𝒄. 𝒎𝒂𝒙 Spatially varying R with result assembly Several workflows allowing a time-accuracy trade off 𝜎 𝑎 and 𝑹 𝝈 𝜎 𝑚𝑖𝑛 𝜎 𝑚𝑎𝑥 𝜎 𝑎 and 𝑹 𝝈 𝜎 𝑚𝑖𝑛 𝜎 𝑚𝑎𝑥 𝜎 𝑎 and 𝑹 𝝈 Force Time 𝑰𝒏𝒄. 𝒊𝒏𝒊𝒕. and 𝑰𝒏𝒄. 𝒆𝒏𝒅 Spatially varying R with full cycle Early design Loading screening Design validation MarcAvailable for :
  • 28. Confidential28 Numerous lifetime corrections to account for stress concentration are available Stress gradient Interpolation Correct stress field and re-compute lifetime II I L 𝝈 𝒆𝒇𝒇. = 𝝈 𝒂𝒕 𝑳 No correction Same results as FEA simulation based on stress field Lifetime averaging Average lifetime predictions in log domain over a given volume Stress averaging Average stress over a given volume and re-compute lifetime Stress gradient Linear averaging I II2L 𝝈 𝒆𝒇𝒇. = 𝟏 𝟐𝑳 න 𝟐𝑳 𝝈𝒅𝒙 Correct stress field and re-compute lifetime Stress gradient Tangent I II 𝝈 𝒆𝒇𝒇. = 𝝈 𝒎𝒂𝒙 𝟏 + 𝑳 𝝈 𝒎𝒂𝒙 𝒅𝝈 𝒅𝒙 Correct stress field and re-compute lifetime
  • 29. Confidential29 Digimat-RP provides the right environment for fatigue lifetime computation
  • 30. Confidential30 Use Digimat to reach accurate SFRP fatigue lifetime predictions Dedicated environment for fatigue failure indicator calibration Dedicated environment for fatigue lifetime computation Partner to push limits
  • 31. Confidential31 Benefit from material supplier calibrations • They already feed Digimat-MX database heavily : +27 fatigue material cards in Digimat 2019.1
  • 32. Confidential32 Next steps • What’s new ? → Look at Digimat 2019.1 release webinar • Interested ? → Look at our case study and come to us to learn more • Yet customer ? → Benefit from our capabilities and from material cards present in Digimat-MX • Looking for guidance ? → Benefit from our expertise in testing, calibration and simulation
  • 33. Leverage reinforced plastics durability prediction, from calibration to post-processing Webinar, 18th September 2019 DSM load bracket fatigue demonstrator Thank you! Q&A Pierre Savoyat Digimat Product Manager pierre.savoyat@e-xstream.com Lucien Douven Research Scientist / Design Engineer lucien.douven@dsm.com