Measurement of meso-scale deformations for modelling textile composites

Size: px
Start display at page:

Download "Measurement of meso-scale deformations for modelling textile composites"

Transcription

1 CompTest 2004 Measurement of meso-scale deformations for modelling textile composites P Potluri, D A Perez Ciurezu, R Ramgulam Textile Composites Group University of Manchester Institute of Science & Technology PO Box 88, Manchester M60 1QD, UK

2 Advantages of Textile Composites Textile Preforms: Easy to handle in the dry form Ability to conform to double curvature surfaces Suitable for RTM, thermoforming Through thickness reinforcement in case of 3D textiles Damage tolerance Textile Composites: Superior fracture toughness Lower in-plane moduli Prediction of thermo-mechanical properties an order of magnitude more complex than unidirectional laminates. Mechanical properties sensitive to processing

3 Textile Composites Unidirectional laminates: micro- and macro- scales Textile Composites: additional level: meso-scale D A C B Meso-scale representation: weave repeat & RUC

4 Meso-scale deformations during processing Uniaxial tension: crimp interchange Biaxial tension: tow-compaction, slight reduction in crimp amplitude D compression A C B In-plane shear: change in inter-tow angles, tow cross-section, tow amplitude, fabric thickness Transverse compression: tow compaction, tow flattening, reduction in crimp amplitude

5 Shear test methods constant normal force shear force conventional shear test Bias extension test Picture frame test Biaxial shear: KES tester ±8 o, onset of wrinkles before shear-lock Picture frame: fabric tension not controlled, thread distortion due to normal boundaries at the clamping area, onset of wrinkles Bias extension: convenient, non-uniform shear zones, dominated by tension near the lock-limit, closely represents draping forces

6 Importance of in-plane shear on composite properties Significant changes to fibre orientations, fibre-volume-fractions, laminate thickness Non-orthogonal Repeating unit cell (RUC) RUC geometry varies at each position in a component. Why bias-extension test? Closely represents the draping process Non-uniform shear near the clamps (in a bias extension test) is similar to the effect of blank holders in a forming process Wide-strip bias-extension is closer to the reality

7 Main objectives: To measure constitutive shear properties of textiles to assist mechanics-based drape modelling To measure the tow geometry changes due to shear in order to construct a more realistic RUC B C C A α A b 1 b 2 C C B p a 2

8 Shear load-deformation Bias extension curve on Zwick tensile tester Tensile Test Machine Force N/cm Strain % Force N/cm image analysis computed from global strain 1 Half included angle, α = cos (( 1+ ε ) cosα ) Shear angle: θ = 90 2α ax 0 Shear angle (º)

9 Test Set-up Inexpensive full-field imaging at high magnification

10 Full-field shear analysis of 7.5 cm sample 0g 500g 1000g 1500g 36º 42º 48º 54º 60º 66º 72º 78º 84º 90º

11 Full-field shear analysis of 40 cm sample 0g 500g 1000g 1500g 36º 42º 48º 54º 60º 66º 72º 78º 84º 90º

12 Comparison of flat-bed scanner set-up and Zwick tensile tester Scan against pic ziwick Standard force (N/cm) Zwick tensile test flat-bet scanner Shear angle (º)

13 Computation of shear angle based on fixed & variable zone B Computed fabric width B C C Computed width (mm) y = x R 2 = L A C C B L c Measured width (mm) Measured height of zone B (mm) measured zone B simple model w / Computed fabric width (mm)

14 Computation of corrected shear angle from corrected global strain Tensile Test Machine l c = l w 0 2 Force N/cm image analysis computed from global strain w sinα l c = l ; where, w = w 2 0 sinα 0 1 constant undeformed zone 0.5 reducing undeformed zone Tow slippage close to lock angle Shear angle (º)

15 Bias extension tests on wide samples: grab tensile test Testing with various fabric widths 6 Force(N/cm) ,5 cm 22,5 cm 30 cm 35 cm 40 cm ziwick Shear angle(º)

16 Tow deformation analysis A b 1 b 2 p a 2

17 Tow thickness th22-1 Fabric thickness Tow thickness (mm) th th Shear angle (º) Thickness (mm) Shear angle (º) Tow amplitude Tow spacing A (mm) p (mm) Shear angle (º) Shear angle (º)

18 Measurement of tow width: Scanned image gives a better measurement Tow width in each unit cell can be measured Comparision between cross section and scanner techniques Scanner tow width Cross section toe width 22-1 Cross section tow width 22-2 Cross section tow width 22-3 Tow width(mm) Shear angle (º)

19 Discussion Wide strip bias extension test represents boundary conditions closer to draping. By accounting for undeformed zone, shear angles can be computed from global strain values Tow slippage occurs in case of a standard width sample. This can be minimised in case of a wide-strip test. An inexpensive full-field shear strain measurement technique has been developed. This can potentially be extended to shear strain mapping on a draped surface. Geometric parameters of a deformed unit cell have been measured using microscopic techniques. While tow width can be measured from the scanned image, tow thickness can be obtained from a section. Further work is being carried-out using a stereo-imaging technique. RUC for each unit cell can be constructed based on the shear angle.

SHEAR TENSION COUPLING IN BIAXIAL BIAS EXTENSION TESTS

SHEAR TENSION COUPLING IN BIAXIAL BIAS EXTENSION TESTS SHER TENSION COUPLING IN IXIL IS EXTENSION TESTS P. Harrison *, P. Potluri Department of Mechanical Engineering, James Watt uilding (South), University of Glasgow, Glasgow G 8QQ, U.K. p.harrison@mech.gla.ac.uk

More information

DRAPING SIMULATION. Recent achievements and future trends. Dr. Sylvain Bel LGCIE University Lyon 1

DRAPING SIMULATION. Recent achievements and future trends. Dr. Sylvain Bel LGCIE University Lyon 1 DRAPING SIMULATION Recent achievements and future trends 1 Dr. Sylvain Bel LGCIE University Lyon 1 2 DRAPING SIMULATION Why? How? What? DRAPING SIMULATION WHY? Clamps Punch Fabric Die 1 2 Resin 3 4 Fig.

More information

INVESTIGATION OF THE PROCESSING PARAMETERS OF A 3D WOVEN REINFORCEMENT

INVESTIGATION OF THE PROCESSING PARAMETERS OF A 3D WOVEN REINFORCEMENT INVESTIGATION OF THE PROCESSING PARAMETERS OF A 3D WOVEN REINFORCEMENT Andreas Endruweit, Dhiren K. Modi and Andrew C. Long School of Mechanical, Materials and Manufacturing Engineering, University of

More information

A FINITE ELEMENT MODEL TO PREDICT MULTI- AXIAL STRESS-STRAIN RESPONSE OF CERAMIC MATRIX COMPOSITES WITH STRAIN INDUCED DAMAGE

A FINITE ELEMENT MODEL TO PREDICT MULTI- AXIAL STRESS-STRAIN RESPONSE OF CERAMIC MATRIX COMPOSITES WITH STRAIN INDUCED DAMAGE A FINITE ELEMENT MODEL TO PREDICT MULTI- AXIAL STRESS-STRAIN RESPONSE OF CERAMIC MATRIX COMPOSITES WITH STRAIN INDUCED DAMAGE Daxu Zhang and D. R. Hayhurst School of Mechanical, Aerospace and Civil Engineering,

More information

EXPERIMENTAL EVALUATION OF SHEAR STRENGTH OF WOVEN WEBBINGS

EXPERIMENTAL EVALUATION OF SHEAR STRENGTH OF WOVEN WEBBINGS EXPERIMENTAL EVALUATION OF SHEAR STRENGTH OF WOVEN WEBBINGS Kevin L. Peil +, Ever J. Barbero +, Eduardo M. Sosa* + Department of Mechanical and Aerospace Engineering, West Virginia University (WVU), Morgantown,

More information

Normalisation Of Shear Test Data For Rate- Independent Compressible Fabrics

Normalisation Of Shear Test Data For Rate- Independent Compressible Fabrics Normalisation Of Shear Test Data For Rate- Independent Compressible Fabrics Philip Harrison* 1, Jo Wiggers 2, Andrew C. Long 2 1 University of Glasgow - Room 09 James Watt (South) Building, Materials Engineering

More information

Influence of uniaxial and biaxial tension on meso-scale geometry and strain fields in a woven composite

Influence of uniaxial and biaxial tension on meso-scale geometry and strain fields in a woven composite Composite Structures 77 (7) 45 418 www.elsevier.com/locate/compstruct Influence of uniaxial and biaxial tension on meso-scale geometry and strain fields in a woven composite P. Potluri *, V.S. Thammandra

More information

DEFORMATION PATTERN AND FAILURE CRITERIA OF WOVEN COMPOSITE PREFORM IN GENERAL BIAS EXTENSION

DEFORMATION PATTERN AND FAILURE CRITERIA OF WOVEN COMPOSITE PREFORM IN GENERAL BIAS EXTENSION DEFORMATION PATTERN AND FAILURE CRITERIA OF WOVEN COMPOSITE PREFORM IN GENERAL BIAS EXTENSION B. Zhu 1,2*, T.X. Yu 1, X.M. Tao 2 1 Department of Mechanical Engineering, Hong Kong University of Science

More information

INFLUENCE KINDS OF MATERIALS ON THE POISSON S RATIO OF WOVEN FABRICS

INFLUENCE KINDS OF MATERIALS ON THE POISSON S RATIO OF WOVEN FABRICS ISSN 1846-6168 (Print), ISSN 1848-5588 (Online) ID: TG-217816142553 Original scientific paper INFLUENCE KINDS OF MATERIALS ON THE POISSON S RATIO OF WOVEN FABRICS Željko PENAVA, Diana ŠIMIĆ PENAVA, Željko

More information

Micro-meso draping modelling of non-crimp fabrics

Micro-meso draping modelling of non-crimp fabrics Micro-meso draping modelling of non-crimp fabrics Oleksandr Vorobiov 1, Dr. Th. Bischoff 1, Dr. A. Tulke 1 1 FTA Forschungsgesellschaft für Textiltechnik mbh 1 Introduction Non-crimp fabrics (NCFs) are

More information

MESO-SCALE MODELLING IN THERMOPLASTIC 5-HARNESS SATIN WEAVE COMPOSITE

MESO-SCALE MODELLING IN THERMOPLASTIC 5-HARNESS SATIN WEAVE COMPOSITE MESO-SCALE MODELLING IN THERMOPLASTIC 5-HARNESS SATIN WEAVE COMPOSITE S. Daggumati a*,i. De Baere a, W. Van Paepegem a, J. Degrieck a, J. Xu b, S.V. Lomov b, I. Verpoest b a Ghent University, Dept. of

More information

Effects of mesostructure on the in-plane properties of tufted carbon fabric composites

Effects of mesostructure on the in-plane properties of tufted carbon fabric composites Effects of mesostructure on the in-plane properties of tufted carbon fabric composites CompTest 2011, 14 th February 2011 Johannes W G Treiber Denis D R Cartié Ivana K Partridge j.treiber@cranfield.ac.uk

More information

Stress-strain response and fracture behaviour of plain weave ceramic matrix composites under uni-axial tension, compression or shear

Stress-strain response and fracture behaviour of plain weave ceramic matrix composites under uni-axial tension, compression or shear Xi an 2-25 th August 217 Stress-strain response and fracture behaviour of plain weave ceramic matrix composites under uni-axial tension compression or shear Heyin Qi 1 Mingming Chen 2 Yonghong Duan 3 Daxu

More information

MULTI-SCALE MODELLING OF FIBRE BUNDLES

MULTI-SCALE MODELLING OF FIBRE BUNDLES THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS MULTI-SCALE MODELLING OF FIBRE BUNDLES N. D. Chakladar 1, P. Mandal 1 *, P. Potluri 2 1 School of Mechanical, Aerospace and Civil Engineering,

More information

Some Proposed Experimental Tests for use in Finite Element Simulation of Composite Forming

Some Proposed Experimental Tests for use in Finite Element Simulation of Composite Forming Some Proposed Experimental Tests for use in Finite Element Simulation of Composite Forming B.K. Cartwright 1, P. de Luca 2, J. Wang 3, K. Stellbrink 4, R. Paton 1 1 Cooperative Research Centre for Advanced

More information

Wiggers, Joram (2007) Analysis of textile deformation during preforming for liquid composite moulding. PhD thesis, University of Nottingham.

Wiggers, Joram (2007) Analysis of textile deformation during preforming for liquid composite moulding. PhD thesis, University of Nottingham. Wiggers, Joram (2007) Analysis of textile deformation during preforming for liquid composite moulding. PhD thesis, University of Nottingham. Access from the University of Nottingham repository: http://eprints.nottingham.ac.uk/10414/1/jw_thesis_final.pdf

More information

DEVELOPMENT OF THERMOELASTIC STRESS ANALYSIS AS A NON-DESTRUCTIVE EVALUATION TOOL

DEVELOPMENT OF THERMOELASTIC STRESS ANALYSIS AS A NON-DESTRUCTIVE EVALUATION TOOL DEVELOPMENT OF THERMOELASTIC STRESS ANALYSIS AS A NON-DESTRUCTIVE EVALUATION TOOL S. Quinn*, R.K. Fruehmann and J.M. Dulieu-Barton School of Engineering Sciences University of Southampton Southampton SO17

More information

Coupling of plasticity and damage in glass fibre reinforced polymer composites

Coupling of plasticity and damage in glass fibre reinforced polymer composites EPJ Web of Conferences 6, 48 1) DOI: 1.151/epjconf/1648 c Owned by the authors, published by EDP Sciences, 1 Coupling of plasticity and damage in glass fibre reinforced polymer composites R. Kvale Joki

More information

Transactions on Engineering Sciences vol 21, 1998 WIT Press, ISSN

Transactions on Engineering Sciences vol 21, 1998 WIT Press,   ISSN Micromechanical modelling of textile composites using variational principles A. Prodromou, Ph. Vandeurzen, G. Huysmans, J. Ivens & I. Verpoest Department ofmetallurgy and Materials Engineering, Katholieke

More information

Module III - Macro-mechanics of Lamina. Lecture 23. Macro-Mechanics of Lamina

Module III - Macro-mechanics of Lamina. Lecture 23. Macro-Mechanics of Lamina Module III - Macro-mechanics of Lamina Lecture 23 Macro-Mechanics of Lamina For better understanding of the macromechanics of lamina, the knowledge of the material properties in essential. Therefore, the

More information

Simulation of wrinkling during textile composite reinforcement forming. Influence of tensile, in-plane shear and bending stiffnesses

Simulation of wrinkling during textile composite reinforcement forming. Influence of tensile, in-plane shear and bending stiffnesses Simulation of wrinkling during textile composite reinforcement forming. Influence of tensile, in-plane shear and bending stiffnesses P. Boisse, N. Hamila, E. Vidal-Sallé, F. Dumont To cite this version:

More information

The bias-extension test for the analysis of in-plane shear properties of textile composite reinforcements and prepregs: a review

The bias-extension test for the analysis of in-plane shear properties of textile composite reinforcements and prepregs: a review The bias-extension test for the analysis of in-plane shear properties of textile composite reinforcements and prepregs: a review P. Boisse, N. Hamila, E. Guzman-Maldonado, A Madeo, G. Hivet, F. Dell Isola

More information

BIAXIAL STRENGTH INVESTIGATION OF CFRP COMPOSITE LAMINATES BY USING CRUCIFORM SPECIMENS

BIAXIAL STRENGTH INVESTIGATION OF CFRP COMPOSITE LAMINATES BY USING CRUCIFORM SPECIMENS BIAXIAL STRENGTH INVESTIGATION OF CFRP COMPOSITE LAMINATES BY USING CRUCIFORM SPECIMENS H. Kumazawa and T. Takatoya Airframes and Structures Group, Japan Aerospace Exploration Agency 6-13-1, Ohsawa, Mitaka,

More information

MODELLING OF DRAPING AND DEFORMATION FOR TEXTILE COMPOSITES

MODELLING OF DRAPING AND DEFORMATION FOR TEXTILE COMPOSITES MODELLING OF DRAPING AND DEFORMATION FOR TEXTILE COMPOSITES A. C. Long, M. J. Clifford, P. Harrison, C. D. Rudd School of Mechanical, Materials, Manufacturing Engineering and Management University of Nottingham,

More information

Strength of GRP-laminates with multiple fragment damages

Strength of GRP-laminates with multiple fragment damages Strength of GRP-laminates with multiple fragment damages S. Kazemahvazi, J. Kiele, D. Zenkert Kungliga Tekniska Högskolan, KTH 100 44 Stockholm, Sweden sohrabk@kth.se SUMMARY The strength of glass fibre

More information

Prediction of Elastic Constants on 3D Four-directional Braided

Prediction of Elastic Constants on 3D Four-directional Braided Prediction of Elastic Constants on 3D Four-directional Braided Composites Prediction of Elastic Constants on 3D Four-directional Braided Composites Liang Dao Zhou 1,2,* and Zhuo Zhuang 1 1 School of Aerospace,

More information

MODELING OF THE BEHAVIOR OF WOVEN LAMINATED COMPOSITES UNTIL RUPTURE

MODELING OF THE BEHAVIOR OF WOVEN LAMINATED COMPOSITES UNTIL RUPTURE MODELING OF THE BEHAVIOR OF WOVEN LAMINATED COMPOSITES UNTIL RUPTURE Jean Paul Charles, Christian Hochard,3, Pierre Antoine Aubourg,3 Eurocopter, 375 Marignane cedex, France Unimeca, 6 rue J. Curie, 3453

More information

4. BEAMS: CURVED, COMPOSITE, UNSYMMETRICAL

4. BEAMS: CURVED, COMPOSITE, UNSYMMETRICAL 4. BEMS: CURVED, COMPOSITE, UNSYMMETRICL Discussions of beams in bending are usually limited to beams with at least one longitudinal plane of symmetry with the load applied in the plane of symmetry or

More information

COMPOSITE REINFORCEMENT FORMING SIMULATION: A MULTISCALE APPROACH

COMPOSITE REINFORCEMENT FORMING SIMULATION: A MULTISCALE APPROACH COMPOSITE REINFORCEMENT FORMING SIMULATION: A MULTISCALE APPROACH N. Hamila A. Khan S. Gatouillat E. De Luycker E. Vidal-Sallé T. Mabrouki P. Boisse Université de Lyon, LaMCoS, INSA-Lyon Philippe.Boisse@insa-lyon.fr

More information

An overview of Carbon Fiber modeling in LS-DYNA. John Zhao October 23 th 2017

An overview of Carbon Fiber modeling in LS-DYNA. John Zhao October 23 th 2017 An overview of Carbon Fiber modeling in LS-DYNA John Zhao zhao@lstc.com October 23 th 2017 Outline Manufacturing of Carbon Fiber Compression molding *MAT_277 & 278 *MAT_293 *MAT_249 Resin transform molding

More information

We are IntechOpen, the first native scientific publisher of Open Access books. International authors and editors. Our authors are among the TOP 1%

We are IntechOpen, the first native scientific publisher of Open Access books. International authors and editors. Our authors are among the TOP 1% We are IntechOpen, the first native scientific publisher of Open Access books 3,350 108,000 1.7 M Open access books available International authors and editors Downloads Our authors are among the 151 Countries

More information

THERMOFORMING SIMULATION OF THERMOPLASTIC TEXTILE COMPOSITES

THERMOFORMING SIMULATION OF THERMOPLASTIC TEXTILE COMPOSITES ECCM6-6 TH EUROPEAN CONFERENCE ON COMPOSITE MATERIALS, Seville, Spain, 22-26 June 204 THERMOFORMING SIMULATION OF THERMOPLASTIC TEXTILE COMPOSITES P. Boisse *, P. Wang, 2, N. Hamila, Laboratoire de Mécanique

More information

QUESTION BANK Composite Materials

QUESTION BANK Composite Materials QUESTION BANK Composite Materials 1. Define composite material. 2. What is the need for composite material? 3. Mention important characterits of composite material 4. Give examples for fiber material 5.

More information

Module-4. Mechanical Properties of Metals

Module-4. Mechanical Properties of Metals Module-4 Mechanical Properties of Metals Contents ) Elastic deformation and Plastic deformation ) Interpretation of tensile stress-strain curves 3) Yielding under multi-axial stress, Yield criteria, Macroscopic

More information

A HOLISTIC APPROACH TO QUALITY MANAGEMENT FOR COMPOSITE FORMING PROCESSES

A HOLISTIC APPROACH TO QUALITY MANAGEMENT FOR COMPOSITE FORMING PROCESSES A HOLISTIC APPROACH TO QUALITY MANAGEMENT FOR COMPOSITE FORMING PROCESSES Dr. Farbod Nezami June 2016 Composite Forming: Reliable, fast, effective, but Geometry Process Source: Airbus, Boeing, ETZ, Daimler

More information

24 th October 2008 Glasgow eprints Service https://eprints.gla.ac.uk

24 th October 2008 Glasgow eprints Service https://eprints.gla.ac.uk Harrison, P. and Wiggers, J. and Long,.C. (008) Normalisation of shear test data for rate-independent compressible fabrics. Journal of Composite Materials 4():pp. 315-344. http://eprints.gla.ac.uk/4650/

More information

BIAS EXTENSION TEST STANDARD

BIAS EXTENSION TEST STANDARD BIAS EXTENSION TEST STANDARD Xiongqi Peng and Jian Cao Advanced Materials Processing Laboratory Department of Mechanical Engineering Northwestern University Evanston, IL August 2003 For Internal Use 1.

More information

INDUSTRIAL FORMING SIMULATION OF MULTI-LAYERED UD NON-CRIMP-FABRICS. 13. LS-DYNA FORUM, , BAMBERG.

INDUSTRIAL FORMING SIMULATION OF MULTI-LAYERED UD NON-CRIMP-FABRICS. 13. LS-DYNA FORUM, , BAMBERG. Sebastian Kreissl, Thomas Senner, Arnulf Lipp, Josef Meinhardt. INDUSTRIAL FORMING SIMULATION OF MULTI-LAYERED UD NON-CRIMP-FABRICS. 13. LS-DYNA FORUM, 07.10.2014, BAMBERG. OUTLINE. BMW i. Production Process

More information

Analysis of parameters influencing the jamming effect in circular braids

Analysis of parameters influencing the jamming effect in circular braids This paper is part of the Proceedings of the 2 International Conference on nd High Performance and Optimum Design of Structures and Materials (HPSM 2016) www.witconferences.com Analysis of parameters influencing

More information

LOCKING AND STABILITY OF 3D TEXTILE COMPOSITE REINFORCEMENTS DURING FORMING

LOCKING AND STABILITY OF 3D TEXTILE COMPOSITE REINFORCEMENTS DURING FORMING 10th International Conference on Composite Science and Technology ICCST/10 A.L. Araújo, J.R. Correia, C.M. Mota Soares, et al. (Editors) IDMEC 015 LOCKING AND STABILITY OF 3D TEXTILE COMPOSITE REINFORCEMENTS

More information

ANALYSIS OF WOVEN REINFORCEMENT PREFORMING USING AN EXPERIMENTAL APPROACH

ANALYSIS OF WOVEN REINFORCEMENT PREFORMING USING AN EXPERIMENTAL APPROACH ANALYSIS OF WOVEN REINFORCEMENT PREFORMING USING AN EXPERIMENTAL APPROACH G. Hivet 1, S. Allaoui 1, D. Soulat 1, A. Wendling 1, S. Chatel 2 1 Institut PRISME/MMH, Université d Orléans, 8 rue Léonard de

More information

ME 582 Advanced Materials Science. Chapter 2 Macromechanical Analysis of a Lamina (Part 2)

ME 582 Advanced Materials Science. Chapter 2 Macromechanical Analysis of a Lamina (Part 2) ME 582 Advanced Materials Science Chapter 2 Macromechanical Analysis of a Lamina (Part 2) Laboratory for Composite Materials Research Department of Mechanical Engineering University of South Alabama, Mobile,

More information

EXPERIMENTAL CHARACTERIZATION AND COHESIVE LAWS FOR DELAMINATION OF OFF-AXIS GFRP LAMINATES

EXPERIMENTAL CHARACTERIZATION AND COHESIVE LAWS FOR DELAMINATION OF OFF-AXIS GFRP LAMINATES 20 th International Conference on Composite Materials Copenhagen, 19-24 th July 2015 EXPERIMENTAL CHARACTERIZATION AND COHESIVE LAWS FOR DELAMINATION OF OFF-AXIS GFRP LAMINATES Esben Lindgaard 1 and Brian

More information

RESPONSE SURFACES OF MECHANICAL BEHAVIOR OF DRY WOVEN FABRICS UNDER COMBINED LOADINGS

RESPONSE SURFACES OF MECHANICAL BEHAVIOR OF DRY WOVEN FABRICS UNDER COMBINED LOADINGS THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS RESPONSE SURFACES OF MECHANICAL BEHAVIOR OF DRY WOVEN FABRICS UNDER COMBINED LOADINGS M. Komeili, A.S. Milani* School of Engineering, University

More information

Modeling and Simulations of Aircraft Structures Stiffness, Damage, and Failure Prediction for Laminated Composites

Modeling and Simulations of Aircraft Structures Stiffness, Damage, and Failure Prediction for Laminated Composites Modeling and Simulations of Aircraft Structures Stiffness, Damage, and Failure Prediction for Laminated Composites H.E.Pettermann 1, C.Schuecker 1, D.H.Pahr 2, F.G.Rammerstorfer 2 1 Austrian Aeronautics

More information

CONTRIBUTIONS TO THE PROCESS MODELLING OF RESIN INFUSION UNDER FLEXIBLE TOOLING (RIFT) MANUFACTURING FOR COMPOSITE AEROSTRUCTURES

CONTRIBUTIONS TO THE PROCESS MODELLING OF RESIN INFUSION UNDER FLEXIBLE TOOLING (RIFT) MANUFACTURING FOR COMPOSITE AEROSTRUCTURES THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS CONTRIBUTIONS TO THE PROCESS MODELLING OF RESIN INFUSION UNDER FLEXIBLE TOOLING (RIFT) MANUFACTURING FOR COMPOSITE AEROSTRUCTURES R.S. Pierce 1

More information

SIMULATION OF THE PREFORMING STEP FOR FLAX DRY WOVEN FABRICS

SIMULATION OF THE PREFORMING STEP FOR FLAX DRY WOVEN FABRICS SIMULATION OF THE PREFORMING STEP FOR FLAX DRY WOVEN FABRICS C. Tephany a*, D. Soulat b, P. Ouagne a, J. Gillibert a a Laboratoire PRISME, Université d Orléans, 8 rue Léonard de Vinci, 45072 Orléans cedex

More information

MAE 322 Machine Design. Dr. Hodge Jenkins Mercer University

MAE 322 Machine Design. Dr. Hodge Jenkins Mercer University MAE 322 Machine Design Dr. Hodge Jenkins Mercer University What is this Machine Design course really about? What you will learn: How to design machine elements 1) Design so they won t break under varying

More information

Non-conventional Glass fiber NCF composites with thermoset and thermoplastic matrices. F Talence, France Le Cheylard, France

Non-conventional Glass fiber NCF composites with thermoset and thermoplastic matrices. F Talence, France Le Cheylard, France 20 th International Conference on Composite Materials Copenhagen, 19-24th July 2015 Non-conventional Glass fiber NCF composites with thermoset and thermoplastic matrices. Thierry Lorriot 1, Jalal El Yagoubi

More information

IMPACT DAMAGE TO 3D WOVEN CFRP COMPOSITE PLATES

IMPACT DAMAGE TO 3D WOVEN CFRP COMPOSITE PLATES IMPACT DAMAGE TO 3D WOVEN CFRP COMPOSITE PLATES G. Zumpano 1,3, MPF Sutcliffe 1, C Monroy Aceves 1, WJ Stronge 1, M. Fox 2 1 Cambridge University Engineering Department Trumpington Street, Cambridge, CB2

More information

FIBRE WAVINESS INDUCED BENDING IN COMPRESSION TESTS OF UNIDERECTIONAL NCF COMPOSITES

FIBRE WAVINESS INDUCED BENDING IN COMPRESSION TESTS OF UNIDERECTIONAL NCF COMPOSITES FIBRE WAVINESS INDUCED BENDING IN COMPRESSION TESTS OF UNIDERECTIONAL NCF COMPOSITES Dennis Wilhelmsson 1, Leif E. Asp 1, Renaud Gutkin 2, Fredrik Edgren 3 1 Chalmers University of Technology, Dept. Industrial

More information

Crash Safety of Lithium-Ion Batteries for Electric Vehicles

Crash Safety of Lithium-Ion Batteries for Electric Vehicles Crash Safety of Lithium-Ion Batteries for Electric Vehicles Elham Sahraei Esfahani Research Scientist, MIT Assistant Professor, GMU Vehicle Crashes and Testing Battery Packs in T Configuration Chevy Volt

More information

MECHANICAL BEHAVIOR OF WOVEN FABRIC COMPOSITES UNDER MESO-LEVEL UNCERTAINTIES: MODELING AND SENSITIVITY ANALYSIS. Mojtaba Komeili

MECHANICAL BEHAVIOR OF WOVEN FABRIC COMPOSITES UNDER MESO-LEVEL UNCERTAINTIES: MODELING AND SENSITIVITY ANALYSIS. Mojtaba Komeili MECHANICAL BEHAVIOR OF WOVEN FABRIC COMPOSITES UNDER MESO-LEVEL UNCERTAINTIES: MODELING AND SENSITIVITY ANALYSIS by Mojtaba Komeili B.Sc. Iran University of Science and Technology, Iran, 2008 A THESIS

More information

Modeling non-isothermal thermoforming of fabricreinforced thermoplastic composites

Modeling non-isothermal thermoforming of fabricreinforced thermoplastic composites Modeling non-isothermal thermoforming of fabricreinforced thermoplastic composites Dominic Schommer, Miro Duhovic, Joachim Hausmann Institut für Verbundwerkstoffe GmbH, Erwin-Schrödinger-Str., Building

More information

GB/T / ISO 527-1:1993

GB/T / ISO 527-1:1993 Translated English of Chinese Standard: GB/T1040.1-2006 www.chinesestandard.net Sales@ChineseStandard.net GB NATIONAL STANDARD OF THE PEOPLE S REPUBLIC OF CHINA ICS 83.080.01 G 31 GB/T 1040.1-2006 / ISO

More information

MODELLING AND SIMULATION OF THE MECHANICAL BEHAVIOUR OF WEFT-KNITTED FABRICS FOR TECHNICAL APPLICATIONS

MODELLING AND SIMULATION OF THE MECHANICAL BEHAVIOUR OF WEFT-KNITTED FABRICS FOR TECHNICAL APPLICATIONS AUTEX Research Journal, Vol. 3, No4, December 003 AUTEX MODELLING AND SIMULATION OF THE MECHANICAL BEHAVIOUR OF WEFT-KNITTED FABRICS FOR TECHNICAL APPLICATIONS Part II: 3D model based on the elastica theory

More information

THERMOELASTIC PROPERTIES PREDICTION OF 3D TEXTILE COMPOSITES

THERMOELASTIC PROPERTIES PREDICTION OF 3D TEXTILE COMPOSITES THERMOELASTI PROPERTIES PREDITION OF 3D TEXTILE OMPOSITES S. P. Yushanov, A. E. Bogdanovich, and M. H. Mohamed 3TEX, Inc., 117 Main ampus Drive, Suite 32, Raleigh, N 2766, U.S.A. SUMMARY: Predictive methodology

More information

DAMAGE MECHANICS MODEL FOR OFF-AXIS FATIGUE BEHAVIOR OF UNIDIRECTIONAL CARBON FIBER-REINFORCED COMPOSITES AT ROOM AND HIGH TEMPERATURES

DAMAGE MECHANICS MODEL FOR OFF-AXIS FATIGUE BEHAVIOR OF UNIDIRECTIONAL CARBON FIBER-REINFORCED COMPOSITES AT ROOM AND HIGH TEMPERATURES DAMAGE MECHANICS MODEL FOR OFF-AXIS FATIGUE BEHAVIOR OF UNIDIRECTIONAL CARBON FIBER-REINFORCED COMPOSITES AT ROOM AND HIGH TEMPERATURES M. Kawai Institute of Engineering Mechanics University of Tsukuba,

More information

Project MMS13 Task 5 Report No 3 (M6/D3)

Project MMS13 Task 5 Report No 3 (M6/D3) Project MMS13 Task 5 Report No 3 (M6/D3) Material Data Requirements and Recommended Test Methods for the Predictive Modelling of Defect Criticality in Composite Material Systems M R L Gower and G D Sims

More information

EXTENSION OF THE PUBLICATION PARADIGM: THE TEXTILE COMPOSITES ARCHIVE

EXTENSION OF THE PUBLICATION PARADIGM: THE TEXTILE COMPOSITES ARCHIVE EXTENSION OF THE PUBLICATION PARADIGM: THE TEXTILE COMPOSITES ARCHIVE John Whitcomb 1, Stepan V. Lomov 2, Andrew Long 3, Jon Crookston 3, Masaru Zako 4, Philippe Boisse 5, Brian C. Owens 1, Dmitry Ivanov

More information

STRUCTURAL EFFICIENCY VIA MINIMISATION OF ELASTIC ENERGY IN DAMAGE TOLERANT LAMINATES

STRUCTURAL EFFICIENCY VIA MINIMISATION OF ELASTIC ENERGY IN DAMAGE TOLERANT LAMINATES ECCM16-16 TH EUROPEAN CONFERENCE ON COMPOSITE MATERIALS, Seville, Spain, 22-26 June 214 STRUCTURAL EFFICIENCY VIA MINIMISATION OF ELASTIC ENERGY IN DAMAGE TOLERANT LAMINATES M. Nielsen a, A. T. Rhead a,

More information

Implementation of a Mesomechanical Material Model for IAD Fabrics within LS-DYNA

Implementation of a Mesomechanical Material Model for IAD Fabrics within LS-DYNA Implementation of a Mesomechanical Material Model for IAD Fabrics within LS-DYNA A 89 MS Special Problems Report Space Systems Design Lab (SSDL) Guggenheim School of Aerospace ngineering Georgia Institute

More information

ANALYSIS OF YARN BENDING BEHAVIOUR

ANALYSIS OF YARN BENDING BEHAVIOUR ANALYSIS OF YARN BENDING BEHAVIOUR B. Cornelissen, R. Akkerman Faculty of Engineering Technology, University of Twente Drienerlolaan 5, P.O. Box 217; 7500 AE Enschede, the Netherlands b.cornelissen@utwente.nl

More information

Slow Velocity Flow Fields in Composite Materials

Slow Velocity Flow Fields in Composite Materials Slow Velocity Flow Fields in Composite Materials A Coupled Problem by the Homogenization Method Noboru Kikuchi and His Associates The University of Michigan Ann Arbor, MI 48109, USA Major Contributors

More information

Open-hole compressive strength prediction of CFRP composite laminates

Open-hole compressive strength prediction of CFRP composite laminates Open-hole compressive strength prediction of CFRP composite laminates O. İnal 1, A. Ataş 2,* 1 Department of Mechanical Engineering, Balikesir University, Balikesir, 10145, Turkey, inal@balikesir.edu.tr

More information

A simplified finite element model for draping of woven material

A simplified finite element model for draping of woven material Composites: Part A 35 (2004) 637 643 www.elsevier.com/locate/compositesa A simplified finite element model for draping of woven material S.B. Sharma, M.P.F. Sutcliffe* Department of Engineering, Cambridge

More information

Development of Novel Skin Materials for Morphing Aircraft

Development of Novel Skin Materials for Morphing Aircraft AFRL-AFOSR-UK-TR-2010-0003 Development of Novel Skin Materials for Morphing Aircraft Venkata P Potluri Universit of Manchester School of Materials Sackville Street Building Manchester, Greater Manchester

More information

Lab Exercise #5: Tension and Bending with Strain Gages

Lab Exercise #5: Tension and Bending with Strain Gages Lab Exercise #5: Tension and Bending with Strain Gages Pre-lab assignment: Yes No Goals: 1. To evaluate tension and bending stress models and Hooke s Law. a. σ = Mc/I and σ = P/A 2. To determine material

More information

FOLDING OF WOVEN COMPOSITE STRUCTURES

FOLDING OF WOVEN COMPOSITE STRUCTURES FOLDING OF WOVEN COMPOSITE STRUCTURES J.C.H. Yee and S. Pellegrino 1 Department of Engineering, University of Cambridge Trumpington Street, Cambridge CB2 1PZ, UK ABSTRACT This paper investigates one-ply

More information

PREDICTING THE CONSTITUTIVE BEHAVIOR OF BIAXIAL BRAIDED COMPOSITES USING BEAM UNIT CELLS

PREDICTING THE CONSTITUTIVE BEHAVIOR OF BIAXIAL BRAIDED COMPOSITES USING BEAM UNIT CELLS THE 19TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS PREDICTING THE CONSTITUTIVE BEHAVIOR OF BIAXIAL 1 J. Cichosz1*, J. Bückle1, R. Hinterhölzl1, M. Wolfahrt2 Institute for Carbon Composites, Technische

More information

Evaluation of in-plane orthotropic elastic constants of paper and paperboard

Evaluation of in-plane orthotropic elastic constants of paper and paperboard Evaluation of in-plane orthotropic elastic constants of paper and paperboard T. Yokoyama and K. Nakai Department of Mechanical Engineering, Okayama University of Science - Ridai-cho, Okayama 7-5, Japan

More information

Chapter 6: Mechanical Properties of Metals. Dr. Feras Fraige

Chapter 6: Mechanical Properties of Metals. Dr. Feras Fraige Chapter 6: Mechanical Properties of Metals Dr. Feras Fraige Stress and Strain Tension Compression Shear Torsion Elastic deformation Plastic Deformation Yield Strength Tensile Strength Ductility Toughness

More information

Modelling the nonlinear shear stress-strain response of glass fibrereinforced composites. Part II: Model development and finite element simulations

Modelling the nonlinear shear stress-strain response of glass fibrereinforced composites. Part II: Model development and finite element simulations Modelling the nonlinear shear stress-strain response of glass fibrereinforced composites. Part II: Model development and finite element simulations W. Van Paepegem *, I. De Baere and J. Degrieck Ghent

More information

In-situ local strain measurement in textile composites with embedded optical fibre sensors

In-situ local strain measurement in textile composites with embedded optical fibre sensors In-situ local strain measurement in textile composites with embedded optical fibre sensors S. Daggumati, E. Voet, I. De Baere, W. Van Paepegem & J. Degrieck Ghent University, Department of Materials Science

More information

PRELIMINARY PREDICTION OF SPECIMEN PROPERTIES CLT and 1 st order FEM analyses

PRELIMINARY PREDICTION OF SPECIMEN PROPERTIES CLT and 1 st order FEM analyses OPTIMAT BLADES Page 1 of 24 PRELIMINARY PREDICTION OF SPECIMEN PROPERTIES CLT and 1 st order FEM analyses first issue Peter Joosse CHANGE RECORD Issue/revision date pages Summary of changes draft 24-10-02

More information

An integrated approach to the design of high performance carbon fibre reinforced risers - from micro to macro - scale

An integrated approach to the design of high performance carbon fibre reinforced risers - from micro to macro - scale An integrated approach to the design of high performance carbon fibre reinforced risers - from micro to macro - scale Angelos Mintzas 1, Steve Hatton 1, Sarinova Simandjuntak 2, Andrew Little 2, Zhongyi

More information

LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS

LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS XXII. LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS Introduction The lamination theory for the elastic stiffness of fiber composite materials is the backbone of the entire field, it holds

More information

Overview of Probabilistic Modeling of Woven Ceramic Matrix Composites ABSTRACT

Overview of Probabilistic Modeling of Woven Ceramic Matrix Composites ABSTRACT ABSTRACT An overview of current research efforts in understanding the cause of variability in the thermo-mechanical properties of woven ceramic matrix composites is presented. Statistical data describing

More information

Composites Science and Technology

Composites Science and Technology Composites Science and Technology 7 (1) 194 1941 Contents lists available at ScienceDirect Composites Science and Technology journal homepage: www.elsevier.com/locate/compscitech Local damage in a 5-harness

More information

Elastic parameters prediction under dynamic loading based on the. unit cell of composites considering end constraint effect

Elastic parameters prediction under dynamic loading based on the. unit cell of composites considering end constraint effect Elastic parameters prediction under dynamic loading based on the unit cell of composites considering end constraint effect Wang Meng 1,, Fei Qingguo 1,, Zhang Peiwei 1, (1. Institute of Aerospace Machinery

More information

Lecture 15 Strain and stress in beams

Lecture 15 Strain and stress in beams Spring, 2019 ME 323 Mechanics of Materials Lecture 15 Strain and stress in beams Reading assignment: 6.1 6.2 News: Instructor: Prof. Marcial Gonzalez Last modified: 1/6/19 9:42:38 PM Beam theory (@ ME

More information

A Stress Gradient Failure Theory for Textile Structural Composites. Final Technical Report submitted to ARO

A Stress Gradient Failure Theory for Textile Structural Composites. Final Technical Report submitted to ARO A Stress Gradient Failure Theory for Textile Structural Composites Final Technical Report submitted to ARO By RYAN KARKKAINEN and BHAVANI SANKAR University of Florida Department of Mechanical & Aerospace

More information

Failure analysis of serial pinned joints in composite materials

Failure analysis of serial pinned joints in composite materials Indian Journal of Engineering & Materials Sciences Vol. 18, April 2011, pp. 102-110 Failure analysis of serial pinned joints in composite materials Alaattin Aktaş* Department of Mechanical Engineering,

More information

Analysis of the mechanical behaviour of woven fibrous material using virtual tests at the unit cell level

Analysis of the mechanical behaviour of woven fibrous material using virtual tests at the unit cell level Analysis of the mechanical behaviour of woven fibrous material using virtual tests at the unit cell level Philippe Boisse, Alain Gasser, Benjamin Hagege, Jean-Louis Billoët To cite this version: Philippe

More information

ME 2570 MECHANICS OF MATERIALS

ME 2570 MECHANICS OF MATERIALS ME 2570 MECHANICS OF MATERIALS Chapter III. Mechanical Properties of Materials 1 Tension and Compression Test The strength of a material depends on its ability to sustain a load without undue deformation

More information

An orthotropic damage model for crash simulation of composites

An orthotropic damage model for crash simulation of composites High Performance Structures and Materials III 511 An orthotropic damage model for crash simulation of composites W. Wang 1, F. H. M. Swartjes 1 & M. D. Gan 1 BU Automotive Centre of Lightweight Structures

More information

3. BEAMS: STRAIN, STRESS, DEFLECTIONS

3. BEAMS: STRAIN, STRESS, DEFLECTIONS 3. BEAMS: STRAIN, STRESS, DEFLECTIONS The beam, or flexural member, is frequently encountered in structures and machines, and its elementary stress analysis constitutes one of the more interesting facets

More information

Plasticity R. Chandramouli Associate Dean-Research SASTRA University, Thanjavur

Plasticity R. Chandramouli Associate Dean-Research SASTRA University, Thanjavur Plasticity R. Chandramouli Associate Dean-Research SASTRA University, Thanjavur-613 401 Joint Initiative of IITs and IISc Funded by MHRD Page 1 of 9 Table of Contents 1. Plasticity:... 3 1.1 Plastic Deformation,

More information

Supplementary Information. Multifunctional graphene woven fabrics

Supplementary Information. Multifunctional graphene woven fabrics Supplementary Information Multifunctional graphene woven fabrics Xiao Li 1, Pengzhan Sun 1, Lili Fan 1, Miao Zhu 1,2, Kunlin Wang 1, Dehai Wu 1, Yao Cheng 2,3 and Hongwei Zhu 1,2* 1 Department of Mechanical

More information

Failure surface according to maximum principal stress theory

Failure surface according to maximum principal stress theory Maximum Principal Stress Theory (W. Rankin s Theory- 1850) Brittle Material The maximum principal stress criterion: Rankin stated max principal stress theory as follows- a material fails by fracturing

More information

MODELLING OF THE THERMO-MECHANICAL PROPERTIES OF WOVEN COMPOSITES DURING THE CURE

MODELLING OF THE THERMO-MECHANICAL PROPERTIES OF WOVEN COMPOSITES DURING THE CURE TH 9 TH INTRNATIONAL ONFRN ON OMPOSIT MATRIALS MODLLING OF TH THRMO-MHANIAL PROPRTIS OF WOVN OMPOSITS DURING TH UR L. Khoun,, K.S. hallagulla,, P. Hubert Department of Mechanical ngineering, McGill University,

More information

Multi Disciplinary Delamination Studies In Frp Composites Using 3d Finite Element Analysis Mohan Rentala

Multi Disciplinary Delamination Studies In Frp Composites Using 3d Finite Element Analysis Mohan Rentala Multi Disciplinary Delamination Studies In Frp Composites Using 3d Finite Element Analysis Mohan Rentala Abstract: FRP laminated composites have been extensively used in Aerospace and allied industries

More information

Fig. 1. Different locus of failure and crack trajectories observed in mode I testing of adhesively bonded double cantilever beam (DCB) specimens.

Fig. 1. Different locus of failure and crack trajectories observed in mode I testing of adhesively bonded double cantilever beam (DCB) specimens. a). Cohesive Failure b). Interfacial Failure c). Oscillatory Failure d). Alternating Failure Fig. 1. Different locus of failure and crack trajectories observed in mode I testing of adhesively bonded double

More information

ANALYSIS OF LOAD FLOW AND STRESS CONCENTRATIONS IN TEXTILE COMPOSITES

ANALYSIS OF LOAD FLOW AND STRESS CONCENTRATIONS IN TEXTILE COMPOSITES 16 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS ANALYSIS OF LOAD FLOW AND STRESS CONCENTRATIONS IN TEXTILE COMPOSITES Deepak Goyal*, John D. Whitcomb*, Julian Varghese* *Department of Aerospace Engineering,

More information

RELATIONSHIP BETWEEN RADIAL COMPRESSIVE MODULUS OF ELASTICITY AND SHEAR MODULUS OF WOOD Jen Y. Liu Research Engineer

RELATIONSHIP BETWEEN RADIAL COMPRESSIVE MODULUS OF ELASTICITY AND SHEAR MODULUS OF WOOD Jen Y. Liu Research Engineer RELATIONSHIP BETWEEN RADIAL COMPRESSIVE MODULUS OF ELASTICITY AND SHEAR MODULUS OF WOOD Jen Y. Liu Research Engineer and Robert J. Ross Supervisory Research Engineer USDA Forest Service Forest Products

More information

EVALUATION OF DAMAGE DEVELOPMENT FOR NCF COMPOSITES WITH A CIRCULAR HOLE BASED ON MULTI-SCALE ANALYSIS

EVALUATION OF DAMAGE DEVELOPMENT FOR NCF COMPOSITES WITH A CIRCULAR HOLE BASED ON MULTI-SCALE ANALYSIS THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS EVALUATION OF DAMAGE DEVELOPMENT FOR NCF COMPOSITES WITH A CIRCULAR HOLE BASED ON MULTI-SCALE ANALYSIS T. Kurashiki 1 *, Y. Matsushima 1, Y. Nakayasu

More information

Enhancing Prediction Accuracy In Sift Theory

Enhancing Prediction Accuracy In Sift Theory 18 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS Enhancing Prediction Accuracy In Sift Theory J. Wang 1 *, W. K. Chiu 1 Defence Science and Technology Organisation, Fishermans Bend, Australia, Department

More information

PLAIN WEAVE REINFORCEMENT IN C/C COMPOSITES VISUALISED IN 3D FOR ELASTIC PARAMETRES

PLAIN WEAVE REINFORCEMENT IN C/C COMPOSITES VISUALISED IN 3D FOR ELASTIC PARAMETRES THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS PLAIN WEAVE REINFORCEMENT IN C/C COMPOSITES VISUALISED IN 3D FOR ELASTIC PARAMETRES P. Tesinova Technical University of Liberec, Faculty of Textile

More information

Chalmers Publication Library

Chalmers Publication Library Chalmers Publication Library Orthotropic criteria for transverse failure of non-crimp fabric-reinforced composites This document has been downloaded from Chalmers Publication Library (CPL). It is the author

More information

STRAIN. Normal Strain: The elongation or contractions of a line segment per unit length is referred to as normal strain denoted by Greek symbol.

STRAIN. Normal Strain: The elongation or contractions of a line segment per unit length is referred to as normal strain denoted by Greek symbol. STRAIN In engineering the deformation of a body is specified using the concept of normal strain and shear strain whenever a force is applied to a body, it will tend to change the body s shape and size.

More information