Finite Element Modeling and Failure Analysis of Roll Bending. Forming of GLARE Laminates

Similar documents
A MODELING METHOD OF CURING DEFORMATION FOR CFRP COMPOSITE STIFFENED PANEL WANG Yang 1, GAO Jubin 1 BO Ma 1 LIU Chuanjun 1

A NUMERICAL SIMULATION OF DAMAGE DEVELOPMENT FOR LAMINATED WOVEN FABRIC COMPOSITES

FINITE ELEMENT ANALYSIS OF A COMPOSITE CATAMARAN

CHAPTER 4. Numerical Models. descriptions of the boundary conditions, element types, validation, and the force

Optimal sensor distribution for impact loading identification

ANALYSIS OF A STRINGER RUN-OUT CONCEPT INCLUDING DAMAGE INITIATION AND EVOLUTION AT THE INTERFACES

COMSOL BASED 2-D FEM MODEL FOR ULTRASONIC GUIDED WAVE PROPAGATION IN SYMMETRICALLY DELAMINATED UNIDIRECTIONAL MULTI- LAYERED COMPOSITE STRUCTURE

Guangxi University, Nanning , China *Corresponding author

Investigating the influence of local fiber architecture in textile composites by the help of a mapping tool

Using Abaqus to Model Delamination in Fiber- Reinforced Composite Materials

ME 475 FEA of a Composite Panel

Study of Convergence of Results in Finite Element Analysis of a Plane Stress Bracket

Comparison of 3-D Fracture Analysis Methods Based on ANSYS Workbench

Computer Life (CPL) ISSN: Finite Element Analysis of Bearing Box on SolidWorks

A Graphical User Interface for Simulating Resin-Transfer-Molding Combining LS-DYNA and OpenFOAM

A numerical study of multi-pass design based on Bezier curve in conventional spinning of spherical components

IJSRD - International Journal for Scientific Research & Development Vol. 3, Issue 07, 2015 ISSN (online):

CHAPTER-10 DYNAMIC SIMULATION USING LS-DYNA

Recent Advances on Higher Order 27-node Hexahedral Element in LS-DYNA

Analysis of fluid-solid coupling vibration characteristics of probe based on ANSYS Workbench

Effectiveness of Element Free Galerkin Method over FEM

ScienceDirect. Forming of ellipse heads of large-scale austenitic stainless steel pressure vessel

SIMULATION OF CARBON-ROVING-STRUCTURES EXTREME LIGHT AND STRONG BY FILAMENT WOUND REINFORCEMENT

An explicit feature control approach in structural topology optimization

STATIC AND DYNAMIC ANALYSIS OF COMPOSITE ROTOR BLADE

Benchmarks for Composite Delamination Using LS-Dyna 971: Low Velocity Impact

Predicting the mechanical behaviour of large composite rocket motor cases

by Mahender Reddy Concept To Reality / Summer 2006

EXACT BUCKLING SOLUTION OF COMPOSITE WEB/FLANGE ASSEMBLY


Reliability Based Design Optimization of Composite Joint Structures

IJMH - International Journal of Management and Humanities ISSN:

STUDY OF PARAMETRIC DESIGN IN DOUBLE-WEDGE CROSS WEDGE ROLLING MODELING. Associate Prof. Xing Xidong, PhD.

Stress Analysis of thick wall bellows using Finite Element Method

Simulation of a Steel Wire Straightening Taking into Account Nonlinear Hardening of Material

Mechanical Behaviors of Non-Crimp Fabric Composites Based on Multi-scale Analysis

inter.noise 2000 The 29th International Congress and Exhibition on Noise Control Engineering August 2000, Nice, FRANCE

Design optimization of C Frame of Hydraulic Press Machine

CHAPTER 1. Introduction

The Dynamic Characteristics Analysis of Rotor Blade Based on ANSYS

Revised Sheet Metal Simulation, J.E. Akin, Rice University

Chapter 1 Introduction

SSR Polygonal Search Area

Effect of the Initial Shape of L-angle Member into Bending Properties on Push-Through Bending of Aluminum Extrusion Section

A Multiple Constraint Approach for Finite Element Analysis of Moment Frames with Radius-cut RBS Connections

Experimental Evaluation and Consideration of Numerical Method of Zanchor CFRP Laminates

II. FINITE ELEMENT MODEL OF CYLINDRICAL ROLLER BEARING

Vehicle Load Area Division Wall Integrity during Frontal Crash

Application of Finite Volume Method for Structural Analysis

Effect of Mesh Size of Finite Element Method in Modal Analysis for Periodic Symmetric Struts Support

Exercise 1. 3-Point Bending Using the GUI and the Bottom-up-Method

A Computational Study of Local Stress Intensity Factor Solutions for Kinked Cracks Near Spot Welds in Lap- Shear Specimens

Finite Element Buckling Analysis Of Stiffened Plates

CHAPTER 6 EXPERIMENTAL AND FINITE ELEMENT SIMULATION STUDIES OF SUPERPLASTIC BOX FORMING

ACTUATING SYSTEMS BASED ON TWO BELLOWS

Modeling and Simulation for Aircraft Structural Repair Using Modern FEA Tools

FAILURE ANALYSIS OF CURVED LAYERED TIMBER CONSTRUCTIONS

NUMERICAL ANALYSIS OF ROLLER BEARING

Influence of geometric imperfections on tapered roller bearings life and performance

COMPUTER AIDED ENGINEERING. Part-1

Example 24 Spring-back

Introduction to Abaqus. About this Course

FE ANALYSES OF STABILITY OF SINGLE AND DOUBLE CORRUGATED BOARDS

Modeling Strategies for Dynamic Finite Element Cask Analyses

First Order Analysis for Automotive Body Structure Design Using Excel

Contents Metal Forming and Machining Processes Review of Stress, Linear Strain and Elastic Stress-Strain Relations 3 Classical Theory of Plasticity

NEW WAVE OF CAD SYSTEMS AND ITS APPLICATION IN DESIGN

Predicting the Elastic Modulus of 3D Braided Composite Tubes Using Geometrical Mapping Approach

Finite Element Analysis of a Sandwich Composite Bicycle Frame

DETECTION AND QUANTIFICATION OF CRACKS IN PRESSURE VESSELS USING ESPI AND FEA MODELLS

Exercise 1. 3-Point Bending Using the Static Structural Module of. Ansys Workbench 14.0

Failure of Notched Laminates Under Out-of- Plane Bending. Phase VI Technical Review John Parmigiani Oregon State University

Mixed Mode Fracture of Through Cracks In Nuclear Reactor Steam Generator Helical Coil Tube

Plane strain conditions, 20 mm thick. b a. Material properties: E aa= N/mm2 Interface properties: G IC=0.28 N/mm E =E 00 N/mm2.

THREE DIMENSIONAL DYNAMIC STRESS ANALYSES FOR A GEAR TEETH USING FINITE ELEMENT METHOD

Element Order: Element order refers to the interpolation of an element s nodal results to the interior of the element. This determines how results can

4D printing method based on the composites with embedded continuous fibers

Guidelines for proper use of Plate elements

Sliding Split Tube Telescope

Optimization Design on Triangle Plate of Auxiliary Frame of Mixer Truck

Engineering Analysis

Finite Element Method. Chapter 7. Practical considerations in FEM modeling

Finite Element Method for Predicting the Behavior of Sandwich Structure Luggage Floor of Passenger Cars

Numerical Calculations of Stability of Spherical Shells

RELIABILITY OF THE FEM CALCULATIONS OF THE FRACTURE MECHANICS PARAMETERS

DEVELOPMENT OF A NUMERICAL MODEL FOR SIMULATIONS OF SPLIT HOPKINSON PRESSURE BAR

Non-Linear Analysis of Bolted Flush End-Plate Steel Beam-to-Column Connection Nur Ashikin Latip, Redzuan Abdulla

SIMULATION CAPABILITIES IN CREO

Deep Beam With Web Opening

FEA Analysis to Study the Influence of Various Forming Parameters on Springback Occurs In Single Point Incremental Forming

Comparison between Experimental and Simulation Results of Bending Extruded Aluminum Profile

The Effect of Element Formulation on the Prediction of Boost Effects in Numerical Tube Bending

Buckling Analysis of a Thin Plate

VIBRATION MONITORING OF COMPOSITE LAMINATES WITH DELAMINATION DAMAGE

Technology), Beijing, , China;

Configuration Optimization of Anchoring Devices of Frame-Supported Membrane Structures for Maximum Clamping Force

Crane Hook Design and Analysis

Modelling Flat Spring Performance Using FEA

Vibration Analysis of Welded Tubular Structures Considering Local Joint Flexibility

Module 1: Introduction to Finite Element Analysis. Lecture 4: Steps in Finite Element Analysis

Transcription:

Finite Element Modeling and Failure Analysis of Roll Bending Forming of GLARE Laminates Jingming Tian, Gang Tao, Cheng Liu, Huaguan Li, Xian Zhang, Jie Tao* College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing city, Jiangsu Province, China Abstract: In this paper, a three-dimensional finite element model of three-roller bending forming process was built under the ABAQUS/Explicit environment based on the solutions of several key techniques, consisting of material property definition, diverse failure criterions, contact boundary condition treatment and meshing technique. Failure characteristics of GLARE in this process were also investigated. Then numerical modeling was used to analyze stress-strain, failure modes and damage characteristics of different laminates. It was found that the failure of epoxy resin matrix occurred with the increase of the displacement of top roller, followed by fiber breakage. Comparison between numerical simulation and experimental tests was provided. Keywords: Hybrid; Laminates; Roll bending forming; Finite element modeling (FEM); Failure 1. Introduction Roll bending forming of GLARE laminates is the most appropriate option for single curved skins [1]. It should be noted that roll bending forming is an efficient technique for forming metal plates into cylindrical or conical shapes due to its simple configuration. Over the years, an extensive investigation was carried out on modeling and simulation for roll bending forming of metal sheets [2-5]. However, published data related with roll bending forming of GLARE laminates are still rather meagre.

Therefore, it is of great worth to investigate roll bending forming of GLARE with FEM simulation to obtain optimized finite element model of roll bending forming of GLARE laminates. Finite element modeling and analysis for roll bending forming of GLARE laminates were primarily indagated in order to make a study of stress and strain, failure of different laminates during roll bending forming. The three-dimensional finite element model was established in this paper with the help of ABAQUS/Explicit & Standard solvers through which the position of the top roller can be predicted accurately. The stress and strain of different GLARE laminates were also investigated. Finally, the results of numerical modeling were compared with experiments. 2. Finite Element Modeling Many key techniques were taken into account including geometry modeling, definition of material properties, contact boundary conditions, mesh and element type to model the roll bending forming of GLARE laminates using ABAQUS/Explicit &Standard solvers [6]. Thus it is necessary to establish constitutive relation and failure model of different GLARE laminates. The finite element model of GLARE laminates employed an independent mesh technique for each layer. Aluminum layers were meshed by three-dimensional eight-node linear brick solid elements, meanwhile, eight-node quadrilateral continuum shell elements were applied for glass/epoxy composite layers. Particularly, a cohesive element was selected to analyze the delamination initiation and propagation of the adhesive layers. The finite element model of roll bending forming of GLARE laminate was built as illustrated in Fig. 1.

Fig. 1The finite element model of roll bending forming of GLARE 3. Results and Discussion The bending strength of GLARE-3/2 laminates after roll bending is shown in Fig. 2(a). Bending strength of finite element simulation is all slightly higher than the experimental value and the error is 3.24%, 4.23% and 4.21%, respectively, totally in the range of 5% allowed by the specification. Thus, the accuracy and reliability of the finite element results are certified. Furthermore, GLARE with 0 /0 configuration show the highest bending modulus after roll bending while GLARE with +45 /-45 configuration show the lowest bending modulus, as shown in Fig. 2(b). It suggests that the ability of bearing bending deformation in the elastic bending deformation stage decreases with the reduction of the content of 0 fiber. Fig. 2 FEM predicted bending strength and bending modulus compared with experiments. (a) bending strength; (b) bending modulus

The main failure mode of the samples after roll bending is matrix fracture and debonding between fibers and matrix, as shown in Fig. 3. Fig. 3 SEM images of cross section for the GLARE samples after roll bending (a) GLARE 2A (b) GLARE 3 (c) GLARE 6A Owing to the existence of 0 fibers in the process of roll bending, GLARE 2A and GLARE 3 possess stronger bending resistance than GLARE 6A. In other words, GLARE 2A and GLARE 3 can bear larger bending deformation during the roll bending process. 4. Conclusions a) An application of finite element model of roll bending forming of GLARE laminates was presented. The ability of bearing bending deformation in the elastic bending deformation stage decreased with the reduction of the content of 0 fiber. And the accuracy and reliability of finite element results were certified. b) SEM results showed that the failure of epoxy resin matrix occurred with the increase of the displacement of top roller, followed by fiber breakage. GLARE 2A and GLARE 3 possessed stronger bending resistance than GLARE 6A.

References [1] Sinke J. Manufacturing of GLARE parts and structures [J]. Applied composite materials, 2003, 10(4-5): 293-305. [2] Yang M, Shima S. Simulation of pyramid type three-roll bending process [J]. International Journal of Mechanical Sciences, 1988, 30(12): 877-886. [3] Feng Z, Champliaud H. Modeling and simulation of asymmetrical three-roll bending process [J]. Simulation Modelling Practice and Theory, 2011, 19(9): 1913-1917. [4] Fan S T, Meng S F. Simulation of the three roll pyramid type plate bending machine: multi-bending process [J]. Machinery Design and Manufacture, 2007, 6: 82-84. [5] Fu Z, Tian X, Chen W, et al. Analytical modeling and numerical simulation for three-roll bending forming of sheet metal [J]. The International Journal of Advanced Manufacturing Technology, 2013, 69(5-8): 1639-1647. [6] Zhao G Y, Liu Y L, Yang H, et al. Three-dimensional finite-elements modeling and simulation of rotary-draw bending process for thin-walled rectangular tube [J]. Materials Science and Engineering: A, 2009, 499(1): 257-261.