Measurement of meso-scale deformations for modelling textile composites
|
|
- Abraham Cunningham
- 5 years ago
- Views:
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
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 informationDRAPING 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 informationINVESTIGATION 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 informationA 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 informationEXPERIMENTAL 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 informationNormalisation 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 informationInfluence 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 informationDEFORMATION 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 informationINFLUENCE 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 informationMicro-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 informationMESO-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 informationEffects 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 informationStress-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 informationMULTI-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 informationSome 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 informationWiggers, 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 informationDEVELOPMENT 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 informationCoupling 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 informationTransactions 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 informationModule 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 informationSimulation 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 informationThe 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 informationBIAXIAL 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 informationMODELLING 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 informationStrength 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 informationPrediction 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 informationMODELING 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 information4. 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 informationCOMPOSITE 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 informationAn 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 informationWe 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 informationTHERMOFORMING 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 informationQUESTION 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 informationModule-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 informationA 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 information24 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 informationBIAS 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 informationINDUSTRIAL 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 informationAnalysis 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 informationLOCKING 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 informationANALYSIS 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 informationME 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 informationEXPERIMENTAL 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 informationRESPONSE 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 informationModeling 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 informationCONTRIBUTIONS 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 informationSIMULATION 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 informationMAE 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 informationNon-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 informationIMPACT 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 informationFIBRE 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 informationCrash 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 informationMECHANICAL 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 informationModeling 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 informationGB/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 informationMODELLING 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 informationTHERMOELASTIC 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 informationDAMAGE 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 informationProject 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 informationEXTENSION 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 informationSTRUCTURAL 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 informationImplementation 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 informationANALYSIS 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 informationSlow 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 informationOpen-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 informationA 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 informationDevelopment 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 informationLab 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 informationFOLDING 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 informationPREDICTING 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 informationEvaluation 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 informationChapter 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 informationModelling 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 informationIn-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 informationPRELIMINARY 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 informationAn 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 informationLAMINATION 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 informationOverview 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 informationComposites 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 informationElastic 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 informationLecture 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 informationA 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 informationFailure 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 informationAnalysis 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 informationME 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 informationAn 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 information3. 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 informationPlasticity 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 informationSupplementary 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 informationFailure 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 informationMODELLING 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 informationMulti 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 informationFig. 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 informationANALYSIS 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 informationRELATIONSHIP 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 informationEVALUATION 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 informationEnhancing 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 informationPLAIN 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 informationChalmers 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 informationSTRAIN. 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