on the experimental modelling of delaminations in composite materials
DESCRIPTION
On the experimental modelling of delaminations in composite materials. C. Devivier, F. Pierron and M. R. Wisnom. Introduction. Dramatic effects from very small impacts Barely visible impact damage (BVID) caused by tool drops BVID involves delaminations Resulting damage pattern is complex. - PowerPoint PPT PresentationTRANSCRIPT
ON THE EXPERIMENTAL MODELLING OF DELAMINATIONS IN COMPOSITE
MATERIALS
C. Devivier, F. Pierron and M. R. Wisnom
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5th CompTest conference14-16 February 2011
Introduction
• Dramatic effects from very small impacts
• Barely visible impact damage (BVID)caused by tool drops
• BVID involves delaminations
• Resulting damage pattern is complex
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Introduction• More simple model
samples with single delaminations
• Test in cantilever bending using grid method by deflectometry
• Issues with artificial delaminations
– in literature PTFE film works for mode I
– in this paper mode II studied
• Objective:
Create a non-destructive evaluation for delaminations
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Dimensions and material
•Simple cantilever beam with a point load
•Samples: 250mm long, 50mm wide and 4mm thick
•32 plies in a quasi-isotropic layup : ([0 45 -45 90]4s)
•Carbon fibre composite (IM7-8552)
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Undamaged
50mm delamination
Samples
Single layer of PTFE(~25µm thick)
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•Distance grid-sample=1.66 m
•Load=5 N
•Grid pitch = 1.5 mm
•7 pixels per grid pitch
•5 Mpix camera with a 28-200mm nikon zoom
•Coated with an opaque resin
Top view
Grid
Camera
Sample
Point load
Experimental set-up
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Unloaded state » 1 picture
Loaded state » 1 picture
Spatial phase shifting (windowed discrete Fourier transform)
-Unloaded state: » Longitudinal » Transverse
-Loaded state: » Longitudinal » Transverse
unloaded state subtracted to loaded state
Strain extraction
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Unwrapping with custom made algorithm.
p: grid pitchh: distance grid-sample
point-to-point differentiation
{}=t/2{}
“Equivalent strains”
Strain extraction
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Resolutions and noise level
In plane: Out of plane:
Resolution in strains:
=6800 µm/m
=2µm/m
x10-3
p: grid pitch (1.5 mm)dx: pixel size(1.5 mm inplane0.7 mm out of plane)
t: specimen thickness (4 mm)
h: distance grid-sample (1600 mm): phase standard deviation (0.01 rad)
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FE model
• Elements– Type: 8-nodes linear elastic brick
– Dimensions: 1 mm x 1 mm x 0.125 mm
– Properties: UD material properties + orientation
• Delaminations:
– Coincident nodes disconnected
– Surface contact introducedto prevent penetrations
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Results (1/4)• To compare correctly experiments and FE
» Same processing
Out-of-planedisplacement
differentiation Slopes
differentiation Curvatures
Scaling:Thin plate theory
Equivalentstrains
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Equivalent strain maps (in m/m)for the undamaged sample (2/4)
Longitudinal strains Transverse strains Twist strains
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Equivalent strain maps (in m/m) for the sample witha single, full width, 50mm-long delamination in the midplane (3/4)
Longitudinal strains Transverse strains Twist strains
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Equivalent strain maps (in m/m)for two impacted samples (4/4)
Longitudinal strains Transverse strains Twist strains
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Conclusion
• Behaviour of artificial delaminations characterized by experimental method.
• Created delamination:
– Good agreement with FE for longitudinal strains,
– Not so good for twist strains,
– Inconclusive for transverse strains because of loading.
• Real impact:
– Indication on damage severity by measurement system
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Future work
• Test on samples with different types of inserts:
– Double layer,
– Different insert material,
– Release agent.
• Find a way to avoid the issue of deforming in plasticity the outer edges.
• Link delamination behaviour with porosity.
• Compare artificially introduced and real impacts in plates.
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Thank you for your attention
Do you have any questions??
[email protected]@chalons.ensam.fr [email protected]