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    Ultrasonic-Assisted Drilling of Glass Fiber Reinforced Composites

    , M.Sc. Thesis Sharif University of Technology Forouzan, Ali (Author) ; Akbari, Javad (Supervisor)
    Abstract
    The fiber-reinforced composite materials possess advantage for structural purpose in various industries. Delamination is recognized as one of the major causes of damage during drilling of fiber reinforced composites, which not only reduces the structural integrity, but also has the potential for long-term performance deterioration. It is difficult to produce precise quality holes with high efficiency by conventional drilling method. Drilling is frequently applied in production cycle while the anisotropy and nonhomogeneity of composite materials affect the chip deformation and machining behavior during drilling. In this thesis, a new non-traditional drilling technology is presented for solve... 

    3-D FEM analysis of plastic behavior inside MMC composites considering damage theory

    , Article 25th Congress of the International Council of the Aeronautical Sciences 2006, Hamburg, 3 September 2006 through 8 September 2006 ; Volume 3 , 2006 , Pages 1759-1768 Abedian, A ; Farahpour, H ; Sharif University of Technology
    Curran Associates Inc  2006
    Abstract
    The delamination phenomenon has been studied in macroscopic scale by different approaches. Here, using micro-mechanical models, it is tried to find the possible relationship between the problem and the stress fields around a fiber. Using the ideas and the results on the free surface cracking of unidirectional composite, the FEM model is developed. The model verification is done by comparing the results by the results obtained in presence of damaged incorporated by the damage theory. Here, on the free surfaces fiber/matrix debonding is applied as a composite damage and the results show a good agreement with the available results  

    Dynamic response of a delaminated composite beam with general lay-ups based on the first-order shear deformation theory

    , Article Composites Part B: Engineering ; Volume 55 , 2013 , Pages 65-78 ; 13598368 (ISSN) Jafari Talookolaei, R. A ; Kargarnovin, M. H ; Ahmadian, M. T ; Sharif University of Technology
    2013
    Abstract
    The dynamic response analysis of a delaminated composite beam with a general lay-up traversed under an arbitrary moving/non-moving force is presented. By employing the energy method and introducing a new finite element, the global mass and stiffness matrices for a Laminated Composite Beam (LCB) of Timoshenko type are derived in which the material couplings (bending-tension, bending-twist, and tension-twist couplings) with the Poisson's effect are considered. In deriving the governing equation the non-penetration condition is imposed by employing the method of Lagrange multipliers. Out of a self-developed finite element program, the natural frequencies and time response of such LCB are... 

    Application of vibration based technique in health monitoring of multi-stable laminated composites

    , Article TIC-STH'09: 2009 IEEE Toronto International Conference - Science and Technology for Humanity, 26 September 2009 through 27 September 2009, Toronto, ON ; 2009 , Pages 170-175 ; 9781424438785 (ISBN) Ghaffari, H ; Saeedi, E ; Zabihollah, A ; Ahmadi, R ; Sharif University of Technology
    Abstract
    This paper deals with the problem of vibration based health monitoring (VHM) in multi-stable asymmetrical laminated composite structures. Multi-stable asymmetrical laminates can be snapped between two or more geometries. The ability of snapping between two or more geometries in multistable composite structures makes them vulnerable to delaminate. Because of these reason early detection of damage in these systems during their service life is receiving increasing attention. In the present work, an efficient and accurate finite element model (FEM) based on layer-wise theory by considering the electro-mechanical coupling effect has been developed to investigate the actuation and /or sensing... 

    Predicting delamination in multilayer composite circuit boards with bonded microelectronic components

    , Article Engineering Fracture Mechanics ; 2017 ; 00137944 (ISSN) Akbari, S ; Nourani, A ; Spelt, J. K ; Sharif University of Technology
    Elsevier Ltd  2017
    Abstract
    The present work developed a mixed-mode cohesive zone model (CZM) with a mode I failure criterion to predict the delamination bending loads of multilayer, composite printed circuit boards (PCBs) assembled with soldered ball grid array (BGA) components that were reinforced with an underfill epoxy adhesive. Two different delamination modes were observed in these microelectronic assemblies: delamination at the interface between the solder mask and the first conducting layer of the PCB, and PCB subsurface delamination at the interface between the epoxy and glass fibers of one of the prepreg layers. The cohesive parameters for each of the two crack paths were obtained from fracture tests of... 

    Exact diffusion-induced elastic fields of a spherical core-shell nano-electrode li-ion battery via spectral theory

    , Article Journal of the Electrochemical Society ; Volume 167, Issue 13 , 2020 Shodja, H. M ; Shahryari, B ; Azizi, P ; Roumi, F ; Sharif University of Technology
    IOP Publishing Ltd  2020
    Abstract
    In Li-ion batteries the interface between the nano-size spherical core graphite and its surrounding solid electrolyte interphase (SEI) layer, just inside SEI is susceptible to damage. Thus, accurate determination of the associated elastic fields is one of the challenges in optimizing the lifetime and capacity of Li-ion batteries. The required precision is achieved by considering the core graphite which belongs to the crystal class D6h as homogeneous spherically isotropic and SEI layer as functionally graded (FG) isotropic material. Moreover, to account for the surface/interface effects appropriately the core-shell nano-structure subjected to the diffusion-induced time-dependent nonuniform... 

    Investigating and Designing Different Parameters of Composite Patch for Damaged Pipe

    , M.Sc. Thesis Sharif University of Technology Ziyarati Yazdeli, Mohammad Hossein (Author) ; Abedian, Ali (Supervisor)
    Abstract
    This paper presents, various parameters of the composite patch for repairing and reinforcement the damaged composite pipe have been investigated. There are various parameters of the composite patch such as Laminate orientation, length, width, material and thickness of the patch. by changing these parameters in each analysis and comparing the results, the optimal patch for the damaged pipe is determined  

    Mixed mode I/II delamination analysis of rubber-modified glass-reinforced epoxy composites

    , Article Journal of Reinforced Plastics and Composites ; Vol. 33, Issue 17 , September , 2014 , pp. 1634-1643 ; ISSN: 07316844 Ghadami, F ; Dadfar, M. R ; Zeraati, A. S ; Sharif University of Technology
    Abstract
    In this study, the effect of carboxyl-terminated butadiene-acrylonitrile liquid rubber on fracture toughness of glass-reinforced epoxy composites has been investigated. Fracture toughness tests were conducted in modes I, II and different mixed mode ratios. The data obtained from these tests have been analyzed by using different methods. Results indicated that interlaminar fracture toughness of composite specimens improved considerably through addition of carboxyl-terminated butadiene-acrylonitrile in modes I, II and mixed mode. Interlaminar fracture surfaces of the specimens were also characterized by field emission scanning electron microscope  

    Development of a Layer-wise Model For Prediction of Interlaminar Crack Growth in Laminated Composites Plates Under Cyclic Loading

    , M.Sc. Thesis Sharif University of Technology Kashani, Hossein (Author) ; Hosseini Kordkheili, Ali (Supervisor)
    Abstract
    In the present work, the beginning and progressive growth of delamination in laminated composites plates has been studied. Interlaminar stresses at free edge of laminate may give rise to edge delamination and result in failure of laminate. So we need to determine the exact interlaminar stresses to predict the failure of laminated composites. A computer code based on layerwise theory that can obtain the exact interlaminar stresses been developed. Comparison between the present study and finite element software result showed the good agreement.A fracture mechanics approach is used to analysis delamination propagation between layers of composites laminate. In this approach damage propagation... 

    A Nonlinear Layerwise Shell Finite Element for Delamination Analysis of Laminated Composite Structures under Large Deformation

    , Ph.D. Dissertation Sharif University of Technology Soltani, Zahra (Author) ; Hosseini Kordkheili, Ali (Supervisor)
    Abstract
    This thesis aims to develop a numerically efficient nonlinear layer-wise shell element formulation for delamination analysis of laminated composite shell structures. The element, in a mesoscale scheme, is formulated based on a zig-zag theory and features three translational degrees of freedom for each node on the mid-surface of the shell in addition with two rotational degrees of freedom for each layer. In this way, the displacement field is formulated via adapting the Mindlin-Reissner theory in each layer and an ordered second-order algorithm for finite rotations. To verify the proposed formulation, many popular benchmark problems for geometric nonlinear analysis of shell problems are... 

    Analysis of Delamination in Fiber-reinforced Composite Laminates Using Multiscale Modeling

    , M.Sc. Thesis Sharif University of Technology Abdolmohammadi, Nafiseh (Author) ; Hosseini Kordkheili, Ali (Supervisor)
    Abstract
    This study presents delamination in fiber-reinforced composite laminates by using multiscale modeling. The meso modeling is used to derive the relationship between microcrack density and damage parameters. Next the selected failure model is applied to analyze the macroscale modeling. The progress of failure terms and the reduction of fiber and matrix properties implemented into ABAQUS/Standard, which enables an individual to create a new material behavior through the user subroutine UMAT. In the following, the contours associated with each of the damage parameters are obtained in each of the damage mode. Then for a specific material, the relationship between microcrack density and damage... 

    Study of Tool Geometry on Ultrasonic Assisted Drilling of Composite Laminates

    , M.Sc. Thesis Sharif University of Technology Mehbudi, Pedram (Author) ; Akbari, Javad (Supervisor)
    Abstract
    Delamination is a major problem in drilling of fiber-reinforced composite materials. Thrust force is an important factor leading to propagation of delamination during drilling process. One of effective methods to reduce machining forces is application of ultrasonic vibrations. In this study ultrasonic assisted drilling is applied to reduce thrust force in drilling of GFRP laminates. In order to conduct experiments a setup is designed and fabricated to apply both vibrations and rotation to drill bits. Using Taguchi method, a set of experiments is conducted with feed rate, spindle speed, point angle and ultrasonic vibration amplitude as control factors. The results show that applying... 

    Investigating the effect of rolling strain on fracture behavior of roll bonded Al6061 laminates under quasi-static and dynamic loading

    , Article Materials Science and Engineering A ; Volume 558 , 2012 , Pages 82-89 ; 09215093 (ISSN) Hosseini Monazzah, A ; Bagheri, R ; Seyed Reihani, S. M ; Sharif University of Technology
    2012
    Abstract
    Damage tolerance improvement has been reported by laminating aluminum alloys and composites by researchers. Three-layer laminates comprising Al6061 outer layers and Al1050 interlayer have been roll bonded in this research. While most of the works done have focused on fracture properties of roll bonded Al laminates in crack arrester geometry, this study explores their behavior in crack divider configuration. Rolling strain is varied to control the interfacial bonding in laminates. The fracture behavior of laminates and the constituent material was examined via three-point bending and impact tests. This study presents significant improvement in damage tolerance of laminates compared to their... 

    High performance Dyneema® fiber laminate for impact resistance/macro structural composites

    , Article Journal of Thermoplastic Composite Materials ; Volume 25, Issue 4 , 2012 , Pages 403-414 ; 08927057 (ISSN) Karbalaie, M ; Yazdanirad, M ; Mirhabibi, A ; Sharif University of Technology
    2012
    Abstract
    UHMWPE composite materials are increasingly used in armors design due to their high strength-to-weight ratios and energy absorption capacities. In this study the effect of production parameters upon the terminal ballistic properties of UHMWPE composite were examined under different conditionings. The composite armor plate laminates were produced by hot pressing with three different pressing times from 10-30 minutes and the laminates conditioned at +115, +125, and +135°C. The molding temperature of SK66 fiber composite has the main direct effect on the ballistic absorption energy, so the relation of molding temperature with the adhesive bonding force between layers, the thickness of the... 

    Dynamics of a generally layered composite beam with single delamination based on the shear deformation theory

    , Article Science and Engineering of Composite Materials ; Volume 22, Issue 1 , 2015 , Pages 57-70 ; 0334181X (ISSN) Jafari Talookolaei, R. A ; Abedi, M ; Kargarnovin, M. H ; Ahmadian, M. T ; Sharif University of Technology
    Walter de Gruyter GmbH  2015
    Abstract
    The free vibration analysis of generally laminated composite beam (LCB) with a delamination is presented using the finite element method (FEM). The effect of material couplings (bending-tension, bending-twist, and tension-twist couplings) with the effects of shear deformation, rotary inertia, and Poisson's effect are taken into account. To verify the validity and the accuracy of this study, the numerical solutions are presented and compared with the results from available references and very good agreement observed. Furthermore, the effects of some parameters such as slenderness ratio, the rotary inertia, the shear deformation, material anisotropy, ply configuration, and delamination... 

    Dynamic analysis of generally laminated composite beam with a delamination based on a higher-order shear deformable theory

    , Article Journal of Composite Materials ; Volume 49, Issue 2 , 2015 , Pages 141-162 ; 00219983 (ISSN) Jafari Talookolaei, R. A ; Abedi, M ; Kargarnovin, M. H ; Ahmadian, M. T ; Sharif University of Technology
    SAGE Publications Ltd  2015
    Abstract
    In this study, the dynamic response of the laminated composite beam with arbitrary lay-ups has been investigated within the framework of the third-order shear deformation theory using the finite element method. A new three-nodded finite element compliant with the theory is introduced next. To deal with the dynamic contact between the delaminated segments, unilateral contact constraints are employed in conjunction with Lagrange multiplier method. Furthermore, the Poisson's effect is incorporated in the formulation of the beam constitutive equation. Also, the higher-order inertia effects and material couplings (flexure-tensile, flexure-twist and tensile-twist couplings) are considered in the... 

    The influence of fiber/matrix debonding on inelastic micro-mechanical behavior of cross-ply IMC composites

    , Article ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis, ESDA2010, 12 July 2010 through 14 July 2010, Istanbul ; Volume 4 , 2010 , Pages 197-222 ; 9780791849187 (ISBN) Teimouri, H ; Abedian, A ; Sharif University of Technology
    2010
    Abstract
    In this study the effect of stress field on delamination and fiber/ matrix debonding in laminated composite panels is investigated from the micro-mechanical point of view by means of 3-D Finite Element Models. Specifically, the behavior of two-layer cross-ply symmetric laminates made up of SCS-6/Ti-24Al-11Nb Intermetallic Matrix Composite (IMC) during cooling from the processing temperature is studied. The results show that large plastic strains occur at the fiber/ matrix interface at the fiber end on the laminate free edge which may eventually extend to the interface of the layers of the laminate inflicting delamination damage. This phenomenon is more serious at the corner areas of the... 

    Vibration based damage detection in smart non-uniform thickness laminated composite beams

    , Article TIC-STH'09: 2009 IEEE Toronto International Conference - Science and Technology for Humanity, 26 September 2009 through 27 September 2009, Toronto, ON ; 2009 , Pages 176-181 ; 9781424438785 (ISBN) Ghaffari, H ; Saeedi, E ; Zabihollah, A ; Ahmadi, R ; Sharif University of Technology
    Abstract
    Laminated composite beams with non-uniform thickness are being used as primary structural elements in a wide range of advanced engineering applications. Tapered composite structures, formed by terminating some of the plies, create geometry and material discontinuities that act as sources for delamination initiation and propagation. Any small damage or delamination in these structures can progress rapidly without any visible external signs. Due to this reason early detection of damage in these systems during their service life is receiving increasing attention. The presence of a crack in a component or structure leads to changes in its global dynamic characteristics results in decreases in... 

    Influence of interfacial adhesion on the damage tolerance of Al6061/SiCp laminated composites

    , Article Ceramics International ; Volume 43, Issue 2 , 2017 , Pages 2632-2643 ; 02728842 (ISSN) Hosseini Monazzah, A ; Pouraliakbar, H ; Jandaghi, M. R ; Bagheri, R ; Seyed Reihani, S. M ; Sharif University of Technology
    Elsevier Ltd  2017
    Abstract
    In this study, lamination as extrinsic mechanism was considered to enhance damage tolerance of three-layer Al6061-5%vol. SiCp/Al1050/Al6061-5%vol. SiCp composites. To fabricate laminates of dissimilar interfacial adhesion, different rolling strains were applied during hot roll-bonding. The discrepancy in interfacial strength of laminates was examined by shear test while toughness values were studied using three-point bending test. It was revealed that both interfacial adhesion and damage tolerance were influenced by rolling strain. Interfacial bonding played the major role in the energy absorption during fracture which was quantified as initiation, propagation and total toughness. The... 

    Molecular dynamics simulation of plastic deformation and interfacial delamination of NiTi/Ag bilayer by cyclic-nanoindentation: Effects of crystallographic orientation of substrate

    , Article Computational Materials Science ; Volume 168 , 2019 , Pages 229-245 ; 09270256 (ISSN) Fazeli, S ; Sadrnezhaad, S. k ; Sharif University of Technology
    Elsevier B.V  2019
    Abstract
    This paper presents a comparative study of plasticity and fracture behavior of the NiTi/Ag bilayer for the different crystallographic orientations of the substrate. Molecular dynamic (MD) simulation was used to determine the deformation mechanism, dislocation density, plastic energy dissipation and delamination of the NiTi/Ag bilayers near the interface, when NiTi aligned at (1 0 0), (1 1 1), (1 1 0), (3 2 1), (2 1 0) and (2 1 1) faces during the cyclic-nanoindentation test. The Griffith energy balance model was used to estimate the energy release associated with the delamination. The results of the simulation are suggested the dependence of deformation mechanism, energy release rate (Gin),...