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Department of Mechanical and Manufacturing Engineering SHEAR STRENGTH MEASUREMENT ON METAL/POLYMER INTERFACE USING FRAGMENTATION TEST S. Charca, O. T. Thomsen Department of Mechanical and Manufacturing Engineering Aalborg University, Aalborg Denmark CompTest 2011, Lausanne
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Department of Mechanical and Manufacturing Engineering Overview Introduction Objectives Sample manufacturing and experimental procedure Results and analysis Filament failure mode Photoelasticity and isochromatic fringe patterns Fragment lengths Finite element analysis validation Conclusions
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Department of Mechanical and Manufacturing Engineering Introduction The mechanical properties and performance of polymer composites materials are to a large extent determined by the interface properties. There are several methods that are currently used to characterize the interface properties such as single fibre pull-out, micro-tension, micro- indentation and fragmentation tests. The single fibre fragmentation test method appears to offer some advantages compared with other methods (e.g. single fiber pull out and micro indentation tests) for assessing the fiber-resin interface shear strength. Moreover it offers the advantage over the other methods that the number of fragments that can be obtained from one single test specimen is typically large, thus enabling a complete statistical analysis. The fragmentation test was proposed initially by Kelly and Tyson (1965) based on their work on tungsten fibres embedded in a Cu matrix.
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Department of Mechanical and Manufacturing Engineering The low cost and high mechanical properties of the steel filament/cord compared to the traditional carbon/glass fibers are the main motivation to the start exploring the potential and reliable application of polymers reinforced by steel filament/cord for civil engineering, automotive, wind turbine and others applications A significant “challenge” in polymers reinforced by steel filament/cord is the resin-steel interface properties Introduction ( cont. )
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Department of Mechanical and Manufacturing Engineering Objectives The objectives of this research include: Study the interface properties of single steel filament embedded in a resin. Achieve multiple fragmentations of steel filaments embedded in an unsaturated polyester matrix. Determination of the failure mechanisms. Perform a statistical analysis including a data discrimination process. And finally to determine the interface shear strength using the Kelly and Tyson criterion.
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Department of Mechanical and Manufacturing Engineering Sample manufacturing Steel filaments: Zinc coated ultra high strength steel filament D = 0.1mm Sizing: Silane with amino functionality Resin: Unsaturated polyester Samples were manufactured by casting using treated (sizing) and non treated filaments 10 dogbone samples were manufactured for each type of filament - 5 samples were made at the Risø DTU National Laboratory for Sustainable Energy (Denmark) facilities and the rest at the AAU facilities
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Department of Mechanical and Manufacturing Engineering Specimens design From the E Crit. and rules of mixture. Where: Fiber fragmentation occurs if: Minimum sample cross section for fragmentation test Fiber Matrix uf um Composite ultm ultf E Crit Obtained at 0.05mm/min Fragmentation occurs if: E < E Crit
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Department of Mechanical and Manufacturing Engineering In order to fix the filament into the mould in the manufacturing process and avoid non uniform stress distribution along the filament; filaments were pre- loaded in tension during the casting and curing process using a 200g weight 220 mm30mm R70 mm 20 mm 15 mm 6 mm Final sample dimensions
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Department of Mechanical and Manufacturing Engineering Experimental setup Fragmentation processes were monitored using the photoelasticity technique, with a 50X magnification stereomicroscope After samples fails, the specimens were polished until to obtain a mirror surface to observe and measure the filament fragments Loading rate: 0.05mm/min
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Department of Mechanical and Manufacturing Engineering Filament failure in the resin displayed a defined pattern as shown using 50X magnification Filament failure mode DB PN CN CN-F DB ---- Debonding PN ---- Partially Necking CN ---- Completely Necking CN-F ---- Completely Necking & Fracture
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Department of Mechanical and Manufacturing Engineering Fragmentation Photoelasticity and isochromatic fringes Typical stress/strain curve on dogbone fragmentation specimens and the corresponding polarization image observed during the test @ ~5.33% Light areas appears around the filament, which is an indication of apparent interface debonding
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Department of Mechanical and Manufacturing Engineering Photoelastic birefringence around the filament fragments at ~37N/mm 2 and ~ 5.70% Microscopic image at ~37N/mm 2 and ~ 5.70%. (Non treated steel filament) In the fragmentation experiments high intensity fringe patterns were observed (light or dark, depending of the polarization angle). High stress concentration zones Matrix is purely subjected to tension
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Department of Mechanical and Manufacturing Engineering Fragment length data discrimination ave1 ave2 ave3 ave4 L eff A 2 <A 4 <A 1 <A 3 Dependent on the specimen cross sectional area, distinct differences in the number of fragments per specimen unit length were observed In the zones 2, 4, and 1 the saturation limit was reached and the samples failed Longer fragment lengths were observed in zone 3 than in the other zones. Accordingly, the fragment lengths in zone 3 have been dismissed from the data processing The observed fragmentation data shows three different length ranges: ~0.5 – 5mm ~5 – 8mm ~8 – 15mm Filament fragment representation along the sample
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Department of Mechanical and Manufacturing Engineering Detailed statistical fitting tests (Kolmogorov-Smirnov and Chi-square) showed that the fragment length distributions for each specimen fitted with the “extreme distributions” (Gamma, Gumbel and Weibull). Histograms show the relative frequencies of occurrence of different fragment lengths. Non-treated filament surface no. of fragments: 284 Treated filament surface no. of fragments: 329
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Department of Mechanical and Manufacturing Engineering Summary of results of the fragmentation test after data discrimination The apparent interface shear strengths were calculated using the Kelly and Tyson relation considering the critical fragment length Non-treated filament surface Treated filament surface
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Department of Mechanical and Manufacturing Engineering ANSYS 12.1 Assumption: Material is linear elastic Element type: 2D plane183 (Axi- symmetric 32000 elements) Perfect interface bonding assumed Thermal analogy for resin shrinkage FEA modeling ult = 3016 N/mm 2 (Steel) Calculated critical fragment length for filament failure using FEA: L cFEA = 1.65mm Experimental average fragment length: L cExp = 1.70mm Filament under study
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Department of Mechanical and Manufacturing Engineering Conclusions Fragmentation tests were successfully implemented with single steel filaments embedded in polyester resin. The fragmentation process start with debonding, followed by necking (yielding) and finally fracture of the steel filaments. Filament fragmentation starts to develop at specimen longitudinal strains exceeding ~4.90%. Fragmentation length distributions fit the “extreme distributions” (Gamma, Gumbel and Weibull). The apparent interface shear strengths derived using the Kelly and Tyson equation are very large. The experimentally observed critical fragment length was confirmed using Finite Element Analysis Apparent improvement of the interface shear strength was observed for samples manufactured using surface treated steel filaments
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Department of Mechanical and Manufacturing Engineering Acknowledgement The research reported was sponsored by the Danish National Advanced Technology Foundation. The financial support is gratefully acknowledged. The authors wish to thank Dr. Jakob I. Bech, Dr. Hans Lilholt, Mr. Tom L. Andersen, Dr. R.T. Durai Prabhakaran and other colleagues at Risø National Laboratory for Sustainable Energy, Technical University of Denmark, for inspiring discussions
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