N o n l i n e a r M u l t i - S c a l e M o d e l i n g o f A e r o s p a c e C o m p o s i t e s M a t e r i a l s & S t r u c t u r e s
|
|
- Benjamin McDonald
- 5 years ago
- Views:
Transcription
1 N o n l i n e a r M u l t i - S c a l e M o d e l i n g o f A e r o s p a c e C o m p o s i t e s M a t e r i a l s & S t r u c t u r e s R o g e r A. A s s a k e r C E O, e - X s t r e a m e n g i n e e r i n g C h i e f M a t e r i a l S t r a t e g i s t, M S C S o f t w a r e Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 1
2 Composites Material Mix 2
3 3 Material Challenges Manage Material Data Generate Data (Cost & Time of Test) Manage, Trace, Protect (IP) Comply (Regulation) Model (composite) Materials, part & systems Nonlinearity: Progressive damage & failure Anisotropy Heterogeneity Process dependency
4 Systems Parts Materials Event 1 Event n Mat n System Use Actual Part (IP Protected) Mat 1 Use Actual Material Model (IP Protected) Parts Use Actual System (IP protected) Use Actual Material Model (IP Protected) Mat n Materials Use Actual System (IP protected) Use Actual Part (IP Protected) Mat 1
5 5 Data Import/Export/Access Search/Compare/Validate Trace/Protect Accurate Predictive CAE Neutral High Fidelity FEA Material Virtual Material Eng. Predict Multi-Materials Multi-Physics Process Automation Capture Processes Automate Processes
6 Exploiting Materials in Systems Design 3rd Party DB s Test Data Fit/Excel MaterialCenter Export Simulation.dll Reports Solvers Input / Characterization Materials Management Utilization
7 E-XSTREAM ENGINEERING Copyright e-xstream engineering, 2011 CONFIDENTIAL 7
8 e-xstream, The material modeling company Software & Engineering company 100% focused on advanced material modeling. Founded in 2003 A team of 30 (+ 4 TBH) 2 offices in Europe + MSC Hybrid sales channel 200+ major customers CAGR of 56% An MSC Software Company (Sep 2012) Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 8
9 Customers Material Suppliers Plastics Composites, Automotive OEMs Tier 1 Aerospace Aero Structures (OEMs) Aero Engines Electric & Electronic Electronic Appliances: Electric : Connectors, transformers Defense Medical Devices Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 9
10 DIGIMAT, The material modeling platform Is The nonlinear multi-scale material modeling platform Used by Material Engineers Structural Engineers At Material Suppliers Tier 1 (Material Users/Any Industry) OEM (Material Users/Any Industry) For Material Engineering Accurate & Efficient FEA of Composite Structures Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 10
11 DIGIMAT Material Engineering Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 11
12 Nonlinear MicroMechanics Mean Field Finite Element E Global behavior Σ ( x) H : E r Localization r r a) b) c c ) : ( r Averaging ε r Local phase behavior r cr : r σ r Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 12
13 Process Material Structure Material Processing Injection molding Compression modling D-LFT Material Microsturcure Chopped fibers Nano,... Material Chracteristics Mechanical Thermal Electric,... Structural Performance Stiffness Strength Fatigue, Material Processing Drapage, AFP, PCM HP-CRTM Material Microsturcure Continuous fibers: UD/Woven Nano,... Material Chracteristics Mechanical Thermal Electric,... Structural Performance - Stiffness - Fatigue, Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 13
14 Nonlinear Multi-Scale Modeling Fibers Stress Carbon Fiber E 1 = 220 GPa E 2 = 15 Gpa G 12 = 22 GPa ν 23 = 0.2, ν 12 = 0.2 Smax =5.400 GPa Fully Coupled NL MicroMech Constituent Prop Process Effect Real MicroStr Micro Failure Matrix Strain Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 14
15 Motivation for Multi-Scale Modeling Continuous Fibers/Draping Carbon Fiber E 1 = MPa E 2 = Mpa G 12 = MPa ν 23 = 0.2 ν 12 = 0.2 Failure Epoxy UD Woven Failure CF Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 15
16 DIGIMAT Structural Engineering Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 16
17 Nonlinear Multi-Scale Modeling Microstructure & Macro Strain Macro Stress & Stiffness Matrix Micro stress, strain, failure 17
18 Structure Engineering Material Engineering Material & Structural Engineering Promising Material Candidates Improved MF Modeling Composite behavior Constituents Behavior Constituents Behavior Draping Inj. Molding Strong, 2-Way Coupling Copyright e-xstream engineering, CONFIDENTIAL
19 C a s e S t u d i e s MATERIAL ENGINEERING Copyright e-xstream engineering, 2011 CONFIDENTIAL 19
20 Mechanical: Stiffness Matrix of CFRP Source: Copyright e-xstream engineering, 2011 CONFIDENTIAL 20
21 Thermal: Thermal Conductivity Materials : thermal conductivity (isotropic) Kerimid 601: 0.23 W/mK Al 2 O 3 : 30.7 W/mK 2-phase Microstructure : Kerimid matrix with Al 2 O 3 fibers matrix : Kerimid inclusions : Al 2 O 3 fibers volume fraction : from 0.0 to 0.4 AR = 6 orientation : random in xy-plane (Random2D) Copyright e-xstream engineering,
22 Electric : Electric Conductivity Materials : electrical conductivity (isotropic) PE: 2.5 E-14 S/cm Carbon : 50 S/cm (effective particle*) Microstructure : 2-phase matrix : PE inclusions : Carbon VF: 0 50% AR: 1, 5.5 & 33 Orientation: Random3D * value obtained from composite with inclusion volume fraction 1.0 [Cai] 22
23 23 Curing of CFRP Defects generated in the material during processing Can eventually lead to failure of the composite Segmentation Matrix enrichment Pores Delamination
24 Curing of CFRP 24
25 25 Curing Analysis of CFRP DIGIMAT enables us to perform in depth studies of complex and realistic microstructures. As an invest into the future we base our simulation approach on the DIGIMAT software, both for our research and the education of a new generation of simulation engineers who will be experts in the modeling of materials. Prof. Vasily Ploshikhin, Airbus endowed chair for Integrative Simulation and Engineering of Materials and Processes (
26 C a s e S t u d i e s MATERIAL ENGINEERING Copyright e-xstream engineering, 2011 CONFIDENTIAL 26
27 Imposed force history Aero Structure: Barely Visible Damage CFRP 4-side clamped plate: Width : 4 in. (100 mm) Length : 6 in. (150 mm) Lay-up sequence : [45/90/-45/0] 3s 24 layers of UD Total thickness : 4.8 mm Materials : Carbon AS4 (source: Hexcel composites, Longitudinal Young s modulus : MPa Transverse Young s modulus : 6220 MPa Transverse shear modulus : 7600 MPa Tensile strength : 4278 MPa Epoxy 15 parts Bisphenol A-epichlorhydrine, 2 parts tri-ethylenetetramine (source: Rensselaer Polytechnic Institute, Troy, New York) Stress-Strain curve for Epoxy ElastoPlastic behavior : 35 Young s modulus : 1300 MPa Yield stress : 22.5 MPa Isotropic exponential hardening Microstructure : Unidirectionnal fibers Volume fraction of fibers = 57 % Stress (%) Strain (%) Experiment Exponential hardening model Force (N) Time Copyright e-xstream engineering, 2011 CONFIDENTIAL 27
28 Aero Structure: Barely Visible Damage in CFRP (Accumulated Plastic Strain in Epoxy Matrix) Copyright e-xstream engineering, 2011 CONFIDENTIAL 28
29 Bird Impact on Composite Belly Fairing UD Woven Failure Epoxy Carbon Fiber E 1 = MPa E 2 = Mpa G 12 = MPa ν 23 = 0.2 ν 12 = 0.2 Failure CF Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 29
30 Bird Impact: Composite Belly Fairing Copyright e-xstream engineering, 2011
31 Macro & Micro Failure Indicators 31
32 32 Aero Engine: Ti/SiC Compressor Blade Turbine Blade: Centrifugal Cyclic Loading Material: Matirx : Ti- ElastoPlastic Reinforcements: SiC Elastic Short Fibers/Oriented
33 OUTLOOK Copyright e-xstream engineering, 2011 CONFIDENTIAL 33
34 Outlook Materials Long Fibers Thermoplastics Woven Composites Performance Fatigue Source: Lomov & Al. Chopped Fiber Continuous Fiber Creep Physics (longer term) More focus on electric conductivity (MD) Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 34
35 CONCLUSIONS Copyright e-xstream engineering, 2011 CONFIDENTIAL 35
36 M U L T I Digimat s Holistic Multi-Scale Modeling Materials Chopped Fibers: Short/Long Continuous Fibers Fillers Physics (Thermo)-Mechanical Thermal Electric Manufacturing Injection Draping Compression Performance Stiffness Strength Fatigue Technology Linear/Nonlinear Mean Field/FEA Micro/Hybrid
37 Digimat Value Proposition e-xstream is the Composite in: Design & Process of Composite Products Copyright e-xstream engineering, 2012 e-xstream CONFIDENTTAL 37
DIGIMAT for NANO-COMPOSITES
DIGIMAT for NANO-COMPOSITES Document Version 2.0.1, February 2010 info@e-xstream.com www.e-xstream.com Materials: Engineering Plastics, Reinforced Plastics, Mineral and Clay fillers. e-xstream Technology:
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 informationMulti-Scale Modeling of Crash & Failure of Reinforced Plastics Parts with DIGIMAT to LS-DYNA interface
7 th European LS-DYNA Conference Multi-Scale Modeling of Crash & Failure of Reinforced Plastics Parts with DIGIMAT to LS-DYNA interface L. Adam, A. Depouhon & R. Assaker e-xstream engineering S.A.. 7,
More informationDigimat material model for short fiber reinforced plastics at Volvo Car Corporation
Digimat material model for short fiber reinforced plastics at Volvo Car Corporation Mats Landervik DYNAmore Nordic Johan Jergeus Volvo Car Corporation June 2, 2015 26TH SICOMP CONFERENCE, GOTHENBURG 1
More informationAnisotropic modeling of short fibers reinforced thermoplastics materials with LS-DYNA
Anisotropic modeling of short fibers reinforced thermoplastics materials with LS-DYNA Alexandre Hatt 1 1 Faurecia Automotive Seating, Simplified Limited Liability Company 1 Abstract / Summary Polymer thermoplastics
More informationMESH MODELING OF ANGLE-PLY LAMINATED COMPOSITE PLATES FOR DNS AND IPSAP
16 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS MESH MODELING OF ANGLE-PLY LAMINATED COMPOSITE PLATES FOR DNS AND IPSAP Wanil Byun*, Seung Jo Kim*, Joris Wismans** *Seoul National University, Republic
More informationRUNWAY DEBRIS IMPACT ON GENERIC COMPOSITE TURBOFAN BLADE MULTISCALE PROGRESSIVE FAILURE ANALYSIS
RUNWAY DEBRIS IMPACT ON GENERIC COMPOSITE TURBOFAN BLADE MULTISCALE PROGRESSIVE FAILURE ANALYSIS Gong Huiling 1 Frank Abdi 2 Marc VillàMontero 2 Cody Godines 2 1 MVT Group Inc, Shanghai, China 2 Alpha
More informationRelease Notes Digimat 6.0.1
Release Notes Digimat 6.0.1 May 2015 p. 2 p. 3 p.4 p. 6 p. 7 p. 9 - p.10 1 P a g e C o p y r i g h t M S C S o f t w a r e B e l g i u m, 2015 New Capabilities Failure indicators o Temperature dependent
More informationVALIDATION of CoDA SOFTWARE for COMPOSITES SYNTHESIS AND PRELIMINARY DESIGN (or GETTING COMPOSITES USED - PART 2 )
VALIDATION of CoDA SOFTWARE for COMPOSITES SYNTHESIS AND PRELIMINARY DESIGN (or GETTING COMPOSITES USED - PART 2 ) Graham D Sims and William R Broughton Composites Design Data and Methods, Centre for Materials
More informationSOME RESEARCH ON FINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS
Mechanical Testing and Diagnosis ISSN 2247 9635, 2012 (II), Volume 3, 79-85 SOME RESEARCH ON FINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS Valeriu DULGHERU, Viorel BOSTAN, Marin GUŢU Technical University
More informationComputational Analysis for Composites
Computational Analysis for Composites Professor Johann Sienz and Dr. Tony Murmu Swansea University July, 011 The topics covered include: OUTLINE Overview of composites and their applications Micromechanics
More informationMECHANICAL FAILURE OF A COMPOSITE HELICOPTER STRUCTURE UNDER STATIC LOADING
MECHANICAL FAILURE OF A COMPOSITE HELICOPTER STRUCTURE UNDER STATIC LOADING Steven Roy, Larry Lessard Dept. of Mechanical Engineering, McGill University, Montreal, Québec, Canada ABSTRACT The design and
More informationMatteo Basso *, Ahmed Elmarakbi. d Arco, Italy
International Conference on Automotive Composites ICAutoC 2016 A. Elmarakbi and A.L. Araújo (Editors) IDMEC 2016 Multiscale Analysis of the Mechanical Performance improvement of composites CFRP laminates,
More informationPREDICTION OF TENSILE STIFFNESS AND FAILURE OF CARBON FIBRE COMPOSITE LAMINAE: A MULTI-SCALE NON-DETERMINISTIC APPROACH
Athens, Greece, 24-28 th June 2018 1 PREDICTION OF TENSILE STIFFNESS AND FAILURE OF CARBON FIBRE COMPOSITE LAMINAE: A MULTI-SCALE NON-DETERMINISTIC APPROACH F. Malgioglio 1,2*, F. Mesquita 2, C. Breite
More informationA STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS
Xi an, 2-25 th August 217 A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS LI Zhongyang 1, LI Dong 2 Mailbox72-35, Yanliang District, Xian, China, Email: zhongyangli@live.com Keywords:
More informationAuthors: Correspondence: ABSTRACT:
Multi-Scale Modeling of the Impact and Failure of Fiber Reinforced Polymer Structures using DIGIMAT to LS-DYNA Interface Authors: L. Adam, R. Assaker & R. Ramaya e-xstream engineering S.A. 7, Rue du Bosquet.
More informationDAMAGE SIMULATION OF CFRP LAMINATES UNDER HIGH VELOCITY PROJECTILE IMPACT
18 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS DAMAGE SIMULATION OF CFRP LAMINATES UNDER HIGH VELOCITY PROJECTILE IMPACT A. Yoshimura 1*, T. Okabe, M. Yamada 3, T. Ogasawara 1, Y. Tanabe 3 1 Advanced
More informationA coupled field finite element model to predict actuation properties of piezoelectrically actuated bistable composites.
A coupled field finite element model to predict actuation properties of piezoelectrically actuated bistable composites. P.F.Giddings, C.R.Bowen, H.A.Kim University of Bath, UK Dept. Mech. ng, University
More informationIn Situ Ultrasonic NDT of Fracture and Fatigue in Composites
ECNDT 26 - Mo.2.6.5 In Situ Ultrasonic NDT of Fracture and Fatigue in Composites I. SOLODOV, K. PFLEIDERER, and G. BUSSE Institute for Polymer Testing and Polymer Science (IKP), Non-destructive Testing
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 informationMicromechanical analysis of FRP hybrid composite lamina for in-plane transverse loading
Indian Journal of Engineering & Materials Sciences Vol. 15, October 2008, pp. 382-390 Micromechanical analysis of FRP hybrid composite lamina for in-plane transverse loading K Sivaji Babu a *, K Mohana
More information12/8/2009. Prof. A.K.M.B. Rashid Department of MME BUET, Dhaka
Prof. A.K.M.B. Rashid Department of MME BUET, Dhaka Introduction and classes of properties Case studies showing selection of the right material for the job Deformation of material under the action of a
More informationThe influence of fiber undulation on the mechanical properties of FRP-laminates. Christian Fiebig, Michael Koch
URN (Paper): urn:nbn:de:gbv:ilm1-2014iwk-099:3 58 th ILMENAU SCIENTIFIC COLLOQUIUM Technische Universität Ilmenau, 08 12 September 2014 URN: urn:nbn:de:gbv:ilm1-2014iwk:3 The influence of fiber undulation
More informationMICROMECHANICAL ANALYSIS OF FRP COMPOSITES SUBJECTED TO LONGITUDINAL LOADING
MICROMECHANICAL ANALYSIS OF FRP COMPOSITES SUBJECTED TO LONGITUDINAL LOADING N. Krishna Vihari 1, P. Phani Prasanthi 1, V. Bala Krishna Murthy 2* and A. Srihari Prasad 3 1 Mech. Engg. Dept., P. V. P. Siddhartha
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 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 informationImpact and Crash Modeling of Composite Structures: A Challenge for Damage Mechanics
Impact and Crash Modeling of Composite Structures: A Challenge for Damage Mechanics Dr. A. Johnson DLR Dr. A. K. Pickett ESI GmbH EURO-PAM 99 Impact and Crash Modelling of Composite Structures: A Challenge
More informationFig. 1. Circular fiber and interphase between the fiber and the matrix.
Finite element unit cell model based on ABAQUS for fiber reinforced composites Tian Tang Composites Manufacturing & Simulation Center, Purdue University West Lafayette, IN 47906 1. Problem Statement In
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 informationNUMERICAL SIMULATION OF DAMAGE IN THERMOPLASTIC COMPOSITE MATERIALS
5 th European LS-DYNA Users Conference Composites NUMERICAL SIMULATION OF DAMAGE IN THERMOPLASTIC COMPOSITE MATERIALS Kevin Brown 1, Richard Brooks, Nicholas Warrior School of Mechanical, Materials and
More informationArchetype-Blending Multiscale Continuum Method
Archetype-Blending Multiscale Continuum Method John A. Moore Professor Wing Kam Liu Northwestern University Mechanical Engineering 3/27/2014 1 1 Outline Background and Motivation Archetype-Blending Continuum
More informationMULTI-SCALE MODELING OF TRIAXIAL WOVEN FABRICS. APPLICATION TO SATELLITE ANTENNA
MULTI-SCALE MODELING OF TRIAXIAL WOVEN FABRICS. APPLICATION TO SATELLITE ANTENNA JEAN-SEBASTIEN GERARD 1, STEPHANE CATALAO 2, ROGER ASSAKER 2, JULIAN SANTIAGO PROWALD 3 1 e-xstream engineering SA, Rue
More informationFinite element analysis of drilled holes in uni-directional composite laminates using failure theories
American Journal of Science and Technology 2014; 1(3): 101-105 Published online May 30, 2014 (http://www.aascit.org/journal/ajst) Finite element analysis of drilled holes in uni-directional composite laminates
More informationNanoindentation of Fibrous Composite Microstructures: Experimentation and Finite Element Investigation. Mark Hardiman
Nanoindentation of Fibrous Composite Microstructures: Experimentation and Finite Element Investigation Mark Hardiman Materials and Surface Science Institute (MSSI), Department of Mechanical and Aeronautical
More informationUSE OF DIGITAL IMAGE CORRELATION TO OBTAIN MATERIAL MODEL PARAMETERS FOR COMPOSITES
USE OF DIGITAL IMAGE CORRELATION TO OBTAIN MATERIAL MODEL PARAMETERS FOR COMPOSITES Brian Croop, Hubert Lobo (DatapointLabs, USA). Presenter: Hubert Lobo, President SUMMARY The development of material
More informationISSN: ISO 9001:2008 Certified International Journal of Engineering Science and Innovative Technology (IJESIT) Volume 2, Issue 4, July 2013
Delamination Studies in Fibre-Reinforced Polymer Composites K.Kantha Rao, Dr P. Shailesh, K. Vijay Kumar 1 Associate Professor, Narasimha Reddy Engineering College Hyderabad. 2 Professor, St. Peter s Engineering
More informationPREDICTION OF OPEN HOLE COMPRESSIVE FAILURE FOR QUASI-ISOTROPIC CFRP LAMINATES BY MMF/ATM METHOD
HE 19 H INERNAIONAL CONFERENCE ON COMPOSIE MAERIALS PREDICION OF OPEN HOLE COMPRESSIVE FAILURE FOR QUASI-ISOROPIC CFRP LAMINAES BY MMF/AM MEHOD. Hioki 1*, M. Nakada 2, Y. Miyano 2, H. Katoh 3 1 Graduate
More informationDevelopment of a code to generate randomly distributed short fiber composites to estimate mechanical properties using FEM
International Journal of Theoretical and Applied Mechanics. ISSN 0973-6085 Volume 12, Number 4 (2017) pp. 863-872 Research India Publications http://www.ripublication.com Development of a code to generate
More information1. Introduction. 2. Testing strategy. Daniel HUELSBUSCH 1, Frank WALTHER 1
6th International Symposium on NDT in Aerospace, 12-14th November 2014, Madrid, Spain - www.ndt.net/app.aerondt2014 More Info at Open Access Database www.ndt.net/?id=16947 Damage detection and fatigue
More informationFINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS
FINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS Ever J. Barbero Department of Mechanical and Aerospace Engineering West Virginia University USA CRC Press Taylor &.Francis Group Boca Raton London New York
More informationINTERNATIONAL JOURNAL OF APPLIED ENGINEERING RESEARCH, DINDIGUL Volume 2, No 1, 2011
Interlaminar failure analysis of FRP cross ply laminate with elliptical cutout Venkateswara Rao.S 1, Sd. Abdul Kalam 1, Srilakshmi.S 1, Bala Krishna Murthy.V 2 1 Mechanical Engineering Department, P. V.
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 informationPredicting Failure of Multiangle Composite Laminates
Predicting Failure of Multiangle Composite Laminates Preliminary discussion (not in textbook): Micromechanics failure analyses vs Macromechanics failure analyses Fiber Architecture of Some Common Composite
More informationComposite models 30 and 131: Ply types 0 and 8 calibration
Model calibration Composite Bi-Phase models 30 and 3 for elastic, damage and failure PAM-CRASH material model 30 is for solid and 3 for multi-layered shell elements. Within these models different ply types
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 informationA RESEARCH ON NONLINEAR STABILITY AND FAILURE OF THIN- WALLED COMPOSITE COLUMNS WITH OPEN CROSS-SECTION
A RESEARCH ON NONLINEAR STABILITY AND FAILURE OF THIN- WALLED COMPOSITE COLUMNS WITH OPEN CROSS-SECTION H. Debski a*, J. Bienias b, P. Jakubczak b a Faculty of Mechanical Engineering, Department of Machine
More informationAssessment Methods of Mechanical Properties of Composite Materials
Mechanics and Mechanical Engineering Vol. 21, No. 4 (2017) 1005 1018 c Lodz University of Technology Assessment Methods of Mechanical Properties of Composite Materials Monika Kamocka Radoslaw J. Mania
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 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 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 informationnumerical implementation and application for life prediction of rocket combustors Tel: +49 (0)
2nd Workshop on Structural Analsysis of Lightweight Structures. 30 th May 2012, Natters, Austria Continuum damage mechanics with ANSYS USERMAT: numerical implementation and application for life prediction
More informationEffects of Resin and Fabric Structure
Fatigue of Wind Blade Laminates: Effects of Resin and Fabric Structure Details David Miller, Daniel D. Samborsky and John F. Mandell Montana State t University it MCARE 2012 Outline Overview of MSU Fatigue
More informationLife Prediction Methodology for Ceramic Matrix Composites
Life Prediction Methodology for Ceramic Matrix Composites Scott Case and Howard Halverson Materials Response Group Department of Engineering Science and Mechanics Virginia Tech Outline: Micromechanics
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 informationNUMERICAL MODELLING OF COMPOSITE PIN- JOINTS AND EXPERIMENTAL VALIDATION
NUMERICAL MODELLING OF COMPOSITE PIN- JOINTS AND EXPERIMENTAL VALIDATION Fabrice PIERRON*, François CERISIER*, and Michel GRÉDIAC** * SMS/ Département Mécanique et Matériaux, École Nationale Supérieure
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 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 informationExperimentally Calibrating Cohesive Zone Models for Structural Automotive Adhesives
Experimentally Calibrating Cohesive Zone Models for Structural Automotive Adhesives Mark Oliver October 19, 2016 Adhesives and Sealants Council Fall Convention contact@veryst.com www.veryst.com Outline
More informationCrashworthiness of composite structures: Experiment and Simulation
Crashworthiness of composite structures: Experiment and Simulation Francesco Deleo, Bonnie Wade and Prof. Paolo Feraboli (UW) Dr. Mostafa Rassaian (Boeing R&T) JAMS 2010 The Joint Advanced Materials and
More informationA fatigue design methodology for GRP composites in offshore underwater applications
A fatigue design methodology for GRP composites in offshore underwater applications Dr P. A. FRIEZE P A F A Consulting Engineers Limited, Hampton, Middx, UK INTRODUCTION Norsk Hydro Troll C field - floating
More informationMathematical Modelling of a Fault Slip Induced by Water Injection
Mathematical Modelling of a Fault Slip Induced by Water Injection T. S. Nguyen, 1 J.Rutqvist 2 and Y. Gugliemi 2 1 Canadian Nuclear Safety Commission 2 Lawrence Berkeley National Laboratory ComGeo IV Symposium
More informationMODEL VALIDATION AND STRUCTURAL ANALYSIS OF A SMALL WIND TURBINE BLADE
8th International DAAAM Baltic Conference INDUSTRIAL ENGINEERING 19-21 April 2012, Tallinn, Estonia MODEL VALIDATION AND STRUCTURAL ANALYSIS OF A SMALL WIND TURBINE BLADE Pabut, O.; Allikas, G.; Herranen,
More informationPrediction of Micromechanical Behaviour of Elliptical Frp Composites
Prediction of Micromechanical Behaviour of Elliptical Frp Composites Kiranmayee.Nerusu Dept. of Mechanical Engg. P. V. P. Siddhartha Institute of Technology, Vijayawada 520 007, A.P, India. P. Phani Prasanthi
More informationCrash and Impact Simulation of Composite Structures by Using CAE Process Chain
Crash and Impact Simulation of Composite Structures by Using CAE Process Chain Madhukar Chatiri 1, Thorsten Schütz 2, Anton Matzenmiller 3, Ulrich Stelzmann 1 1 CADFEM GmbH, Grafing/Munich, Germany, mchatiri@cadfem.de
More informationPLY WAVINESS ON IN-PLANE STIFFNESS OF COMPOSITE LAMINATES
PLY WAVINESS ON IN-PLANE STIFFNESS OF COMPOSITE LAMINATES Cimini Jr., Carlos A., and Tsai, Stephen W. 2 Department of Mechanical Engineering, Federal University of Minas Gerais Av. Antônio Carlos, 6627
More informationMechanical Properties
Mechanical Properties Elastic deformation Plastic deformation Fracture I. Elastic Deformation S s u s y e u e T I II III e For a typical ductile metal: I. Elastic deformation II. Stable plastic deformation
More informationSTRESS ANALYSIS OF BONDED JOINTS IN PULTRUDED GRP COMPONENTS
16 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS STRESS ANALYSIS OF BONDED JOINTS IN PULTRUDED GRP COMPONENTS S.W. Boyd*, J. M. Dulieu-Barton*, O. T. Thomsen**, A.Gherardi* [J.M. Dulieu-Barton]: janice@soton.ac.uk
More informationAN EXPLORATION OF STRUCTURE DESIGN IN 3D BRAIDED CERAMIC MATRIX COMPOSITES TURBINE BLADE DOVETAIL ATTACHMENT
AN EXPLORATION OF STRUCTURE DESIGN IN 3D BRAIDED CERAMIC MATRIX COMPOSITES TURBINE BLADE DOVETAIL ATTACHMENT Zhen Cheng, Duoqi Shi*, Xin Jing, Xiaoguang Yang 1 School of Energy and Power Engineering, Beihang
More informationKeywords: Adhesively bonded joint, laminates, CFRP, stacking sequence
THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS GLOBAL AND LOCAL INFLUENCE OF STACKING SEQUENCE ON THE STRENGTH OF ADHESIVELY BONDED JOINTS OF CFRP LAMINATES J. Rousseau*, P. Satthamnuwong DRIVE,
More informationAmerican Society for Testing and Materials (ASTM) Standards. Mechanical Testing of Composites and their Constituents
Mechanical Testing of Composites and their Constituents American Society for Testing and Materials (ASTM) Standards Tests done to determine intrinsic material properties such as modulus and strength for
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 informationThe Power of Ultrasonic Characterisation for Completely Assessing the Elastic Properties of Materials
11th European Conference on Non-Destructive Testing (ECNDT 214), October 6-1, 214, Prague, Czech Republic The Power of Ultrasonic Characterisation for Completely Assessing the Elastic Properties of Materials
More informationPREDICTION OF OUT-OF-PLANE FAILURE MODES IN CFRP
PREDICTION OF OUT-OF-PLANE FAILURE MODES IN CFRP R. R. Pinto 1, P. P. Camanho 2 1 INEGI - Instituto de Engenharia Mecanica e Gestao Industrial, Rua Dr. Roberto Frias, 4200-465, Porto, Portugal 2 DEMec,
More informationEffect of Specimen Dimensions on Flexural Modulus in a 3-Point Bending Test
Effect of Specimen Dimensions on Flexural Modulus in a 3-Point Bending Test M. Praveen Kumar 1 and V. Balakrishna Murthy 2* 1 Mechanical Engineering Department, P.V.P. Siddhartha Institute of Technology,
More informationNUMERICAL DESIGN OF COMPOSITE MATERIALS THROUGH MULTI-SCALE COMPUTER SIMULATION
THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS NUMERICAL DESIGN OF COMPOSITE MATERIALS THROUGH J. Leach 1 *, J. Mackiewicz 2, Dr. S. Risser 1 1 Battelle Memorial Institute, Columbus, OH, USA,
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 information1 332 Laboratories 1. 2 Computational Exercises 1 FEA of a Cantilever Beam... 1 Experimental Laboratory: Tensile Testing of Materials...
1 332 Laboratories Contents 1 332 Laboratories 1 2 Computational Exercises 1 FEA of a Cantilever Beam.......................................... 1 Experimental Laboratory: Tensile Testing of Materials..........................
More informationConstitutive and Damage Accumulation Modeling
Workshop on Modeling and Data needs for Lead-Free Solders Sponsored by NEMI, NIST, NSF, and TMS February 15, 001 New Orleans, LA Constitutive and Damage Accumulation Modeling Leon M. Keer Northwestern
More informationEFFECT OF THERMAL FATIGUE ON INTRALAMINAR CRACKING IN LAMINATES LOADED IN TENSION
EFFECT OF THERMAL FATIGUE ON INTRALAMINAR CRACKING IN LAMINATES LOADED IN TENSION J.Varna and R.Joffe Dept of Applied Physics and Mechanical Engineering Lulea University of Technology, SE 97187, Lulea,
More informationTHREE DIMENSIONAL STRESS ANALYSIS OF THE T BOLT JOINT
THREE DIMENSIONAL STRESS ANALYSIS OF THE T BOLT JOINT Víctor Martínez 1, Alfredo Güemes 2, Norbert Blanco 1, Josep Costa 1 1 Escola Politècnica Superior. Universitat de Girona. Girona, Spain (17071) 2
More informationMaterial Characterization of Carbon Fiber Reinforced Polymer Laminate Using Virtual Fields Method
Proceedings of ICTACEM 014 International Conference on Theoretical, Applied, Computational and Experimental Mechanics December 9-31, 014, IIT Kharagpur, India ICTACEM-014/39 Material Characterization of
More information2 Experiment of GFRP bolt
16 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS FATIGUE LIFE EVALUATION OF BOLT MADE OF WOVEN FABRIC FRP Takeshi INOUE*, Hiroaki NAKAI**, Tetsusei KURASHIKI**, Masaru ZAKO**, Yuji KOMETANI*** *Graduate
More informationA STRAIN-BASED DAMAGE MECHANICS MODELING FOR WOVEN FABRIC COMPOSITES UNDER BIAXIAL FATIGUE LOADING
International Journal of Civil Engineering and Technology (IJCIET) Volume 9, Issue 3, March 2018, pp. 282 291, Article ID: IJCIET_09_03_030 Available online at http://http://www.iaeme.com/ijciet/issues.asp?jtype=ijciet&vtype=9&itype=3
More informationA MULTISCALE DAMAGE MODEL FOR THE ANALYSIS OF LAMINATED COMPOSITE STRUCTURES ON THE MICROSCALE
A MULTISCALE DAMAGE MODEL FOR THE ANALYSIS OF LAMINATED COMPOSITE STRUCTURES ON THE MICROSCALE P. Ladevèze 1,2, M. Trovalet 1, G. Lubineau 1 1 LMT-Cachan (ENS Cachan/CNRS/UPMC/Pres Universud Paris) 61
More informationFatigue Analysis of Wind Turbine Composites using Multi-Continuum Theory and the Kinetic Theory of Fracture
Fatigue Analysis of Wind Turbine Composites using Multi-Continuum Theory and the Kinetic Theory of Fracture P. Greaves a, P. McKeever a, R. G. Dominy b, T. Koziara b a Narec, Offshore House, Albert Street,
More informationMultiscale analyses of the behaviour and damage of composite materials
Multiscale analyses of the behaviour and damage of composite materials Presented by Didier BAPTISTE ENSAM, LIM, UMR CNRS 8006 151 boulevard de l hôpital l 75013 PARIS, France Research works from: K.Derrien,
More informationDamage analysis of composite structures: a software editor point of view and illustration on industrial applications
1 SAMCEF Solver group, SAMTECH s.a., A Siemens Company 2 Aerospace & Mechanical Engineering Dpt, University of Liège Damage analysis of composite structures: a software editor point of view and illustration
More informationCHEM-C2410: Materials Science from Microstructures to Properties Composites: basic principles
CHEM-C2410: Materials Science from Microstructures to Properties Composites: basic principles Mark Hughes 14 th March 2017 Today s learning outcomes To understand the role of reinforcement, matrix and
More informationAim of the study Experimental determination of mechanical parameters Local buckling (wrinkling) Failure maps Optimization of sandwich panels
METNET Workshop October 11-12, 2009, Poznań, Poland Experimental and numerical analysis of sandwich metal panels Zbigniew Pozorski, Monika Chuda-Kowalska, Robert Studziński, Andrzej Garstecki Poznan University
More informationASPECTS CONCERNING TO THE MECHANICAL PROPERTIES OF THE GLASS / FLAX / EPOXY COMPOSITE MATERIAL
5 th International Conference Advanced Composite Materials Engineering COMAT 2014 16-17 October 2014, Braşov, Romania ASPECTS CONCERNING TO THE MECHANICAL PROPERTIES OF THE GLASS / FLAX / EPOXY COMPOSITE
More informationUNIVERSITY OF SASKATCHEWAN ME MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 13, 2008 Professor A. Dolovich
UNIVERSITY OF SASKATCHEWAN ME 313.3 MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 13, 2008 Professor A. Dolovich A CLOSED BOOK EXAMINATION TIME: 3 HOURS For Marker s Use Only LAST NAME (printed): FIRST
More informationMultiscale Approach to Damage Analysis of Laminated Composite Structures
Multiscale Approach to Damage Analysis of Laminated Composite Structures D. Ivančević and I. Smojver Department of Aeronautical Engineering, Faculty of Mechanical Engineering and Naval Architecture, University
More informationProbabilistic fatigue life prediction of multidirectional composite laminates
Composite Structures 69 () 9 www.elsevier.com/locate/compstruct Probabilistic fatigue life prediction of multidirectional composite laminates Yongming Liu, Sankaran Mahadevan * Department of Civil and
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 informationKINK BAND FORMATION OF FIBER REINFORCED POLYMER (FRP)
KINK BAND FORMATION OF FIBER REINFORCED POLYMER (FRP) 1 University of Science & Technology Beijing, China, niukm@ustb.edu.cn 2 Tsinghua University, Department of Engineering Mechanics, Beijing, China,
More informationNUMERICAL MODELING OF GAS LEAKAGE THROUGH DAMAGED COMPOSITE LAMINATES
NUMERICAL MODELING OF GAS LEAKAGE THROUGH DAMAGED COMPOSITE LAMINATES Hisashi Kumazawa*, John Whitcomb** [Hisashi Kumazawa]:kumazawa.hisashi@jaxa.jp *Structure Technology Center, Japan Aerospace Exploration
More informationEffects of geometry and properties of fibre and matrix on overall. composite parameters
Int. Journal of Applied Sciences and ngineering Research, ol. 3, Issue 4, 2014 www.ijaser.com 2014 by the authors Licensee IJASR- Under Creative Commons License 3.0 editorial@ijaser.com Research article
More informationPrediction of Encapsulant Performance Toward Fatigue Properties of Flip Chip Ball Grid Array (FC-BGA) using Accelerated Thermal Cycling (ATC)
Prediction of Encapsulant Performance Toward Fatigue Properties of Flip Chip Ball Grid Array (FC-BGA) using Accelerated Thermal Cycling (ATC) ZAINUDIN KORNAIN 1, AZMAN JALAR 2,3, SHAHRUM ABDULLAH 3, NOWSHAD
More informationBuckling Behavior of 3D Randomly Oriented CNT Reinforced Nanocomposite Plate
Buckling Behavior of 3D Randomly Oriented CNT Reinforced Nanocomposite Plate Outline Introduction Representative Volume Element (RVE) Periodic Boundary Conditions on RVE Homogenization Method Analytical
More informationFracture Mechanics, Damage and Fatigue: Composites
University of Liège Aerospace & Mechanical Engineering Fracture Mechanics, Damage and Fatigue: Composites Ludovic Noels Computational & Multiscale Mechanics of Materials CM3 http://www.ltas-cm3.ulg.ac.be/
More information