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Hugo Faria Marcelo F. S. F. de Moura

Determination of Inter- and Intra-Laminar G Ic and G IIc in GFRP Pipes Using an Hybrid Numerical/Experimental Methodology. Hugo Faria Marcelo F. S. F. de Moura. Porto, Portugal. Faculty of Dental Medicine. Faculty of Psychology. Faculty of Medicine. Faculty of Sport.

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Hugo Faria Marcelo F. S. F. de Moura

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  1. Determination of Inter- and Intra-Laminar GIc and GIIc in GFRP Pipes Using an Hybrid Numerical/Experimental Methodology Hugo Faria Marcelo F. S. F. de Moura ECCM14, Budapest

  2. Porto, Portugal CompTest2011, Lausanne

  3. Faculty of Dental Medicine Faculty of Psychology Faculty of Medicine Faculty of Sport Faculty of Economy INESC Faculty of Engineering INEGI CompTest2011, Lausanne

  4. Overview • Introduction • Background • Numerical/Experimental Methodology • Results • Conclusions • Present and Future Work CompTest2011, Lausanne

  5. Introduction Context • Recent projects conducted by INEGI/FEUP related to GFRP Pipes: • (2000-2005) FP5 Project – “GRP Design & Test” • co-normative project (EN1227; EN1447; EN705; …); • short-, medium- and long-term mechanical tests (<10000h). • (2003-2006) FCT Project – “Previsão Propriedades Longo Prazo Tubagens PRFV” • material characterization tests; • test data extrapolation methods; • numerical modelling. • (2004-2005) MSc Thesis – “Failure Behaviour of GFRP Pipes Under Ring Deflection Loading Condition” • (2008-2010) Real Production Tests • Monitoring and Optimization of the winding of large GFRP pipes CompTest2011, Lausanne

  6. Introduction Objectives • The main objectives of this work are: • correct modelling of the “macroscopic” behaviour of GFRP Pipes up to failure under two loading cases: internal pressure and ring deflection; • correct modelling of the damage phenomena leading to failure at the meso-scale; • determination of the physical parameters governing the damage behaviour; • validation of the ability to develop reallistic models for curved laminates, in view of more complex models and applications. CompTest2011, Lausanne

  7. Background Typical Loading Cases Under-Soil Pipings EN1226 EN1227 Pressurized Flow Pipings EN1447 CompTest2011, Lausanne

  8. Background Composite Laminates Damage Modelling Cohesive Elements σ = D δ σ = ( I – E ) D δ CompTest2011, Lausanne

  9. Numerical/Experimental Methodology Specimens Specifications of the sample pipes used in this study CompTest2011, Lausanne

  10. Numerical/Experimental Methodology Testing Campaigns Internal Pressure Tests CompTest2011, Lausanne

  11. Numerical/Experimental Methodology Testing Campaigns Ring Deflection Tests CompTest2011, Lausanne

  12. Numerical/Experimental Methodology Assumptions 3D model – 1 layer ±α 52,5º 29kg Verification: pipes with 90º oriented layers don’t present edge effects and therefore have longitudinally uniform behaviour 90º Assumption: pipes with 90º oriented layers can be properly modelled in 2D CompTest2011, Lausanne

  13. Numerical/Experimental Methodology Assumptions Assumption: due to the axissymmetry of the pipe section, it can be modelled through an hal-section CompTest2011, Lausanne

  14. Numerical/Experimental Methodology Assumptions Assumption: due to the axissymmetry of the pipe section, it can be modelled through an hal-section CompTest2011, Lausanne

  15. Numerical/Experimental Methodology 2D Models σ = D δ σ = ( I – E ) D δ CompTest2011, Lausanne

  16. Numerical/Experimental Methodology 2D models CompTest2011, Lausanne

  17. Results Ring Deflection buckling of outer plies Progression of fibre rupture through the cross charged section CompTest2011, Lausanne

  18. Results Ring Deflection CompTest2011, Lausanne

  19. Results Internal Pressure CompTest2011, Lausanne

  20. Results Internal Pressure experimental failure CompTest2011, Lausanne

  21. Results Critical Fracture Energies • 0.2 kJ/m2 < GId < 0.3 kJ/m2 • 0.45 < GId / GIId < 0.50 • 400 < GIf/GId < 600 CompTest2011, Lausanne

  22. Conclusions • FEM models able to simulate quantitatively and qualitatively the behaviour of GFRP pipes up to failure under internal pressure and ring deflection loading were successfully established ; • the slope of the “macro-curves” P-d and P-σθ is determined by the elastic-apparent modulus, E1, and the thickness, t; • the “failure initiation” point is determined by GIf , GId e σu; • the experimental/numerical methodology allows an easier determination of the critical values for the energy release rates of these curved laminates CompTest2011, Lausanne

  23. Present and Future Work • experimental measurement of the stress/strain state for comparison; • generalization/validation of the methodology in other types of GFRP pipes and laminates; • generalization/validation of the methodology for other loading cases; • refine the study in order to reduce the range of admissibility for GIf, and GId; CompTest2011, Lausanne

  24. Acknowledgments • Portuguese Foundation for Science and Technology (FCT) • Growth Programme of FP5 (EC) • Prof. Rui M. Guedes CompTest2011, Lausanne

  25. THANK YOU FOR YOUR ATTENTION CompTest2011, Lausanne

  26. ? Discussion Hugo Faria hfaria@inegi.up.pt COMET ModEFil SEAFLOOR CompTest2011, Lausanne

  27. Projects Overview ModEFil Numerical Modelling of the Filament Winding Process CompTest2011, Lausanne

  28. Projects Overview Domestic Gas Container OP: 8 bar | TP: 30 bar | BP: > 60 bar Steel Liner | GF/PP COMET CompTest2011, Lausanne

  29. Projects Overview Hyperbaric Chamber OP: 200 bar | TP: 320 bar | BP: > 600 bar Steel Liner | Biocompatible Internal Layer | CF/Epoxy SEAFLOOR CompTest2011, Lausanne

  30. Projects Overview Water Tank OP: 06 bar | TP: 15 bar RESCOMPRE PE Liner | Metallic Ends | GF/UP CompTest2011, Lausanne

  31. Projects Overview SENSEFIL Online Structural Health Monitoring (SHM) of Composite Overwrapped Pressure Vessels (COPV) CompTest2011, Lausanne

  32. Projects Overview Numerical Simulation of the Failure Behaviour of GFRP Wound Pipes GFRPSIM CompTest2011, Lausanne

  33. Projects Overview Numerical Simulation of the Failure Behaviour of GFRP Wound Pipes GFRPSIM Cohesive Interface Elements CompTest2011, Lausanne

  34. Projects Overview THINCO GF/UP |Thickness: < 250 µm CompTest2011, Lausanne

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