Relevant bibliographies by topics / Laminated composite material

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Laminated composite material'

Author: Grafiati
Published: 4 June 2021
Last updated: 28 January 2023

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Journal articles on the topic "Laminated composite material"

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Dibyajyoti, D., and B. Alfia. "Review on laminated composite plates." Proceedings of the 12th Structural Engineering Convention, SEC 2022: Themes 1-2 1, no. 1 (2022): 83–88. http://dx.doi.org/10.38208/acp.v1.477.

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A composite material is a combination of different material which can be assembled to provide required engineering properties like bending, buckling, stiffness etc. It can give better properties than those of individual components. A lamina is the building block of modern composite laminated structures. A lamina is also known as a ply, or a layer. A laminate has several layers of lamina, or laminae. Since the early years of engineering, various types of laminated composite materials have been used in various engineering fields, such as in aerospace, military and automotive industries that are
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Ramadhan, Redha Akbar, Muhamad Giri Suada, and Hendri Syamsudin. "A FINITE ELEMENT ANALYSIS OF CRITICAL BUCKLING LOAD OF COMPOSITE PLATE AFTER LOW VELOCITY IMPACT." Jurnal Teknologi Dirgantara 18, no. 2 (2020): 195. http://dx.doi.org/10.30536/j.jtd.2020.v18.a3328.

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Composite is a material formed from two or more materials that macroscopically alloyed into one material. Nowadays, composite has been generally applied as lightweight structure of aircraft. This is due to the fact that composites having high strength-to-weight ratio. It means the composites have the capability to take on various loads, despite their lightweight property.Laminate composite is one type of composite that has been generally used in aircraft industries. This type of composite is susceptible to low-velocity impact induced damage. This type of damage can be happening in manufacture,
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Gajbhiye, ParamD, Vishisht Bhaiya, and YuwarajM Ghugal. "Bending Analysis of Orthotropic Plate using 5th Order Shear Deformation Theory." Proceedings of the 12th Structural Engineering Convention, SEC 2022: Themes 1-2 1, no. 1 (2022): 89–94. http://dx.doi.org/10.38208/acp.v1.478.

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A composite material is a combination of different material which can be assembled to provide required engineering properties like bending, buckling, stiffness etc. It can give better properties than those of individual components. A lamina is the building block of modern composite laminated structures. A lamina is also known as a ply, or a layer. A laminate has several layers of lamina, or laminae. Since the early years of engineering, various types of laminated composite materials have been used in various engineering fields, such as in aerospace, military and automotive industries that are
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bin Yaakob, Mohd Yuhazri, T. T. T. Jennise, H. Sihombing, N. Mohamad, S. H. Yahaya, and M. Y. A. Zalkis. "Water Absorption and Thickness Swelling of Laminated Composite after Cured at Different Angle." Applied Mechanics and Materials 465-466 (December 2013): 86–90. http://dx.doi.org/10.4028/www.scientific.net/amm.465-466.86.

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Moisture absorption is a very important factor in polymers and composite materials used for hull manufacture and stability in marine environment. High water absorption of the material will affects the mechanical properties and stability in composite. This research is carried out to study the feasibility of the gravity effects on curing position of the laminated composite structures to enhance the curing space needed. Vertical cured laminate having almost similar properties with common horizontal cured laminate able to save much space in composite industry. Horizontal cured laminates filled up
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Taheri-Behrooz, Fathollah, and Nima Bakhshi. "Neuber’s rule accounting for the material nonlinearity influence on the stress concentration of the laminated composites." Journal of Reinforced Plastics and Composites 36, no. 3 (2016): 214–25. http://dx.doi.org/10.1177/0731684416680302.

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Since holes comprise the necessary features of many structural components, a comprehensive understanding of the behavior of composite plates containing an open hole is a crucial step in their design process. In the present manuscript, an extensive numerical study has been conducted in order to investigate the effects of material nonlinearity on the stress distribution and stress concentration factors in unidirectional and laminated composite materials. To attain this objective, various models with different configurations were studied. In unidirectional composites, the maximum deviation of str
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Fakhruddin, Muhammad, Maskuri Maskuri, Elka Faizal, Bayu Pranoto, Hangga Wicaksono, and Hilmi Iman Firmansyah. "Pengaruh Perlakuan Permukaan Pengikatan Terhadap Sifat Mekanik Komposit Serat Kaca Dengan Laminasi Almunium." Jurnal Energi dan Teknologi Manufaktur (JETM) 4, no. 02 (2021): 27–32. http://dx.doi.org/10.33795/jetm.v4i02.79.

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Fiber metal laminates or commonly known as fiber metal laminates (FML) are composite structures made by combining 2 layers of material as the outer layer with the core material. The outer layer of this composite is called the laminate. Generally, laminated composites are produced by joining techniques under solid-state conditions, such as diffusion bonding, extrusion, friction-stir welding, and roller welding. In this study, glass fiber composites with aluminum lamination were made using the vacuum assisted resin infusion (VARI) method, using epoxy resin. The surface treatment of the aluminum
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bin Yaakob, Mohd Yuhazri, T. T. T. Jennise, H. Sihombing, Qumrul Ahsan, S. T. W. Lau, and Mohd Imran bin Ghazali. "Gravity Effects on the Density of Laminated Composite due to the Differences in Angle Cured." Applied Mechanics and Materials 465-466 (December 2013): 81–85. http://dx.doi.org/10.4028/www.scientific.net/amm.465-466.81.

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This research is carried out to study the feasibility of the gravity effects on curing position of the laminated composite structures to enhance the curing space needed. Vertical cured laminate having almost similar properties with common horizontal cured laminate able to save much space in composite industry especially for developing Small and Medium Industry (SMI). Horizontal cured laminates filled up spaces in which SMI lack of. Polyesters and E-glass fibers were used as the raw material in this research. Vacuum bagging technique was used to suck out the excess resin during lay-up to avoid
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Luo, Shen-Yi, and Faruk Taban. "Deformation of Laminated Elastomer Composites." Rubber Chemistry and Technology 72, no. 1 (1999): 212–24. http://dx.doi.org/10.5254/1.3538791.

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Abstract Flexible elastomer composites subjected to finite deformation are usually associated with significant fiber re-orientation and configuration change which cannot be described by classical composite lamination theory. Utilizing the Lagrangian description and a strain-energy density approach, this work presents a set of 2-D constitutive equations in terms of the overall deformation of laminated composites. This model includes both geometric and material nonlinearities of the laminate. Interlaminar shear deformation is addressed but not studied in this analysis. Theoretical predictions ha
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Luccioni, Bibiana M. "Constitutive Model for Fiber-Reinforced Composite Laminates." Journal of Applied Mechanics 73, no. 6 (2006): 901–10. http://dx.doi.org/10.1115/1.2200654.

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Nowadays, conventional materials have been progressively replaced by composite materials in a wide variety of applications. Particularly, fiber reinforced composite laminates are widely used. The appropriate design of elements made of this type of material requires the use of constitutive models capable of estimating their stiffness and strength. A general constitutive model for fiber reinforced laminated composites is presented in this paper. The model is obtained as a generalization of classical mixture theory taking into account the relations among the strains and stresses in the components
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Xu, Jian, Pei Xian Zhu, Hui Yu Ma, and Sheng Gang Zhou. "Characterisation of Ti-Al and Ti-Cu Laminated Composite Electrode Materials." Advanced Materials Research 194-196 (February 2011): 1667–71. http://dx.doi.org/10.4028/www.scientific.net/amr.194-196.1667.

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We proposed using Ti-Al and Ti-Cu laminated composites instead of single Ti electrode metals, as well as studied the difference in performance between laminated composite electrode materials and pure-Ti electrode. The analysis of the conductivity and electrochemical performance of electrode matrix material indicates the result that the improvement of matrix material by using Ti-Al and Ti-Cu laminated composites, better performance for conductivity of electrode, and be beneficial to homogenize the electrode surface potential and current distribution and promote electrocatalytic activity between
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Dissertations / Theses on the topic "Laminated composite material"

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Teh, Kuen Tat. "Impact damage resistance and tolerance of advanced composite material systems." Diss., This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-06062008-170512/.

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Chandrashekhara, K. "Geometric and material nonlinear analysis of laminated composite plates and shells." Diss., Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/54739.

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An inelastic material model for laminated composite plates and shells is formulated and incorporated into a finite element model that accounts for both geometric nonlinearity and transverse shear stresses. The elasto-plastic material behavior is incorporated using the flow theory of plasticity. In particular, the modified version of Hill's initial yield criterion is used in which anisotropic parameters of plasticity are introduced with isotropic strain hardening. The shear deformation is accounted for using an extension of the Sanders shell theory and the geometric nonlinearity is considered i
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Thielman, Scott C. "Design and optimization of a material property distribution in a laminated composite flywheel /." Thesis, Connect to this title online; UW restricted, 1997. http://hdl.handle.net/1773/7031.

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Rourk, Dave. "Geometric and material nonlinear effects in elastic-plastic and failure analyses of anisotropic laminated structures." Diss., Virginia Polytechnic Institute and State University, 1986. http://hdl.handle.net/10919/76492.

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In this study, an analytical procedure to predict the strength and failure of laminated composite structures under monotonically increasing static loads is presented. A degenerated 3-D shell finite element that includes linear elastic and plastic material behavior with full geometric nonlinearity is used to determine stresses at selected points (Gauss quadrature points in each element) of the structure. Material stiffness (constitutive) matrices are evaluated at each Gauss point, in each lamina and in each element, and when the computed stress state violates a user selected failure criterion,
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Gunel, Murat. "Linear And Nonlinear Progressive Failure Analysis Of Laminated Composite Aerospace Structures." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12614033/index.pdf.

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This thesis presents a finite element method based comparative study of linear and geometrically non-linear progressive failure analysis of thin walled composite aerospace structures, which are typically subjected to combined in-plane and out-of-plane loadings. Different ply and constituent based failure criteria and material property degradation schemes have been included in a PCL code to be executed in MSC Nastran. As case studies, progressive failure analyses of sample composite laminates with cut-outs under combined loading are executed to study the effect of geometric non-linearity on the
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Chee, Clinton Yat Kuan. "STATIC SHAPE CONTROL OF LAMINATED COMPOSITE PLATE SMART STRUCTURE USING PIEZOELECTRIC ACTUATORS �." University of Sydney. Aeronautical Engineering, 2000. http://hdl.handle.net/2123/709.

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The application of static shape control was investigated in this thesis particularly for a composite plate configuration using piezoelectric actuators. A new electro-mechanically coupled mathematical model was developed for the analysis and is based on a third order displacement field coupled with a layerwise electric potential concept. This formulation, TODL, is then implemented into a finite element program. The mathematical model represents an improvement over existing formulations used to model intelligent structures using piezoelectric materials as actuators and sensors. The reason is TOD
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Gordon, Neal A. "Material Health Monitoring of SIC/SIC Laminated Ceramic Matrix Composites With Acoustic Emission And Electrical Resistance." University of Akron / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=akron1414835900.

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Gu, Hanfeng. "Multigrid methods for 3D composite material simulation and crack propagation modelling based on a phase field method." Thesis, Lyon, 2016. http://www.theses.fr/2016LYSEI090/document.

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Avec le développement des techniques d’imagerie telles que la tomographie par rayons X au cours des dernières années, il est maintenant possible de prendre en compte la microstructure réelle dans les simulations des matériaux composites. Cependant, la complexité des composites tels que des fibres inclinées et brisées, les vides, exige un grand nombre des données à l’échelle microscopique pour décrire ces détails et amène ainsi des problèmes difficiles en termes de temps de calcul et de mémoire lors de l’utilisation de méthodes de simulation traditionnelles comme la méthode Eléments Finis. Ces
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Bovicelli, Federico. "On the influence of polymeric nanofibers in laminated composite materials. Studio dell'influenza di nanofibre polimeriche in materiali compositi laminati." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2014. http://amslaurea.unibo.it/6784/.

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During the last years an increased interest about the reinforcement of laminated composites by means of polymeric nanofibers has been growth. During this master-degree-thesis work, unidirectional and plane-textile composites have been interleaved with Nylon 6.6, PCL and mixed (Nylon 6.6+PCL) nanofibrous mats and the DCB (mode I interlaminar fracture toughness), ENF (mode II interlaminar fracture toughness and DMA (damping capability) tests have been performed. Regarding the interlaminar fracture toughness, marked increases have been recorded; while further investigation about damping capabilit
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Padoin, Eduardo. "Otimização topológica de cascas compostas laminadas com atuador piezelétrico para o controle de vibrações." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2014. http://hdl.handle.net/10183/115273.

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Este trabalho apresenta uma metodologia de otimização topológica de atuadores piezelétricos em estruturas compostas laminada com o objetivo de atenuar as vibrações estruturais induzidas por excitações externas. Para isso, utiliza-se técnicas de controle ótimo, como o regulador linear quadrático (LQR) e o controlador linear quadrático gaussiano (LQG). Os estados não mensuráveis são estimados através do uso de observadores de estados de ordem completa, usando o filtro de Kalman para a escolha ótima da matriz de ganhos do observador de estados. O problema de otimização topológica é formulado para
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Books on the topic "Laminated composite material"

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Harris, C. E. Preliminary report on tests of tensile specimens with a part-through surface notch for a filament wound graphite/epoxy material. National Aeronautics and Space Administration, Langley Research Center, 1985.

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Pettermann, Heinz. Derivation and finite element implementation of constitutive material laws for multiphase composites based on Mori-Tanaka approaches. VDI Verlag, 1997.

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Mechanics of composite materials. 2nd ed. Taylor & Francis, 1999.

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R, White S., ed. Stress analysis of fiber-reinforced composite materials. WCB McGraw-Hill, 1998.

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Air Force Wright Aeronautical Laboratories. Cumulative damage model for advanced composite materials. Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1985.

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Reddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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Reddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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Reddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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Reddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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Staab, George H. Laminar composites. Butterworth-Heinemann, 1999.

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Book chapters on the topic "Laminated composite material"

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Borri, A., E. Speranzini, and R. Vetturini. "Optimum Design of Laminated Composite Material Structures." In Computer Aided Design in Composite Material Technology III. Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2874-2_31.

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Adali, Sarp. "Optimization of Laminated Composites and Overview of Smart Material Applications." In Modern Trends in Composite Laminates Mechanics. Springer Vienna, 2003. http://dx.doi.org/10.1007/978-3-7091-2544-1_5.

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Brito, F. M. "The Boundary Between the Concepts of Material and Structure in the Plate and Shell Theories for Laminated Media." In Composite Structures 4. Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3457-3_9.

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Han, J., and S. V. Hoa. "Three Dimensional Composite Elements for Finite Element Analysis of Anistropic Laminated Structures." In Computer Aided Design in Composite Material Technology III. Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2874-2_16.

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Machado, R. D., and C. S. Barcellos. "A First Modified Local Green’s Function Method Approach to Orthotropic Laminated Plates." In Computer Aided Design in Composite Material Technology III. Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2874-2_27.

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Olhoff, Niels, and Bin Niu. "Discrete Material Optimization of Vibrating Laminated Composite Plates for Minimum Sound Emission." In Topology Optimization in Structural and Continuum Mechanics. Springer Vienna, 2014. http://dx.doi.org/10.1007/978-3-7091-1643-2_15.

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Jia, Zehui, Lingwei Xu, Shuangkai Huang, Haoran Xu, Zhimo Zhang, and Xu Cui. "Preparation and Impact Resistance of Carbon Fiber Reinforced Metal Laminates Modified by Carbon Nanotubes." In Lecture Notes in Civil Engineering. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-1260-3_27.

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AbstractFiber reinforced metal laminates (FMLs) are a kind of interlaminar hybrid composites made of metal sheets and fibers alternately stacked and cured at a certain pressure and temperature. In this paper, through the simulation of ABAQUS finite element software and recording the change of projectile velocity, the energy loss of projectile is calculated and the impact resistance is judged. Through the comparison of three groups of simulation experimental results, the energy absorbed by carbon fiber reinforced metal laminate is about 300 times that of aluminum alloy plate, which fully shows that carbon fiber reinforced metal composite has excellent impact resistance compared with aluminum alloy. After adding 1 wt% carbon nanotubes to carbon fiber reinforced metal laminates, the absorbed energy is about 10 times that of the original, which shows that carbon nanotubes improve the ultimate yield stress of resin and materials in epoxy resin and enhance the weakness that the composites are easy to delamination under impact load.
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Muzakkar, M. Z., S. Ahmad, M. A. Yarmo, A. Jalar, and M. Bijarimi. "Shear Strength of Single Lap Joint Aluminium-Thermoplastic Natural Rubber (Al-TPNR) Laminated Composite." In Recent Trends in Physics of Material Science and Technology. Springer Singapore, 2014. http://dx.doi.org/10.1007/978-981-287-128-2_10.

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Groppetti, R., A. Armanni, A. Cattaneo, and G. Franceschini. "Contribution to the Study of the Delamination of Carbon Fibre Reinforced Plastic (CFRP) Laminated Composites during Piercing and Cutting by Hydro Jet Machining (HJM) and Hydro Abrasive Jet Machining (HAJM)." In Computer Aided Design in Composite Material Technology III. Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2874-2_13.

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Le, Quoc-Cuong, and Ba-Duy Nguyen. "Buckling and Vibration Analysis Based on a Novel Unified Model for Laminated Composite Beams." In Proceedings of the 2nd Annual International Conference on Material, Machines and Methods for Sustainable Development (MMMS2020). Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69610-8_57.

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Conference papers on the topic "Laminated composite material"

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Jung, Dongho, Hyeonju Kim, Moonho Tak, Kyungjae Lee, and Taehyo Park. "Dynamic Structural Analysis of a Large-Diameter Riser Consisting of Laminated Composite Material With a Hybrid Numerical Scheme." In ASME 2013 32nd International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/omae2013-10868.

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A hybrid numerical scheme is developed to analyze the structural dynamic behavior of a large-diameter riser made of a laminated composite material. The global dynamic behavior of the riser, considered as a beam element subjected to a wave and current, is solved with the finite element analysis method in the time domain. The equivalent elastic modulus of a laminated composite riser for the global dynamic analysis is calculated from the stress-strain relation of a laminate structure with a different elastic modulus. For elements in large displacement and stresses estimated from the dynamic analy
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Arıko¨k, Rifat, and Zahit Mecitog˘lu. "Large Deflection of a Laminated Composite Plate With Different Extensional and Flexural Material Properties." In ASME 2010 International Mechanical Engineering Congress and Exposition. ASMEDC, 2010. http://dx.doi.org/10.1115/imece2010-40592.

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This paper presents the large deflection elastic analysis of the hand lay-up composite plates with different extensional and flexural modulus including geometric nonlinearity effects that are taken into account with the von Ka´rma´n large deflection theory of thin plates. Governing equations of the motion are derived by means of the virtual work principle. Then the Galerkin method is applied to reduce the nonlinear coupled differential equations into a nonlinear algebraic equation system. The MATLAB and MATHEMATICA software are used to solve the equation system. Because of the common nonunifor
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Vinogradov, Aleksandra M. "Buckling Characteristics of Regular and Irregular Asymmetric Laminated Composites." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-0883.

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Abstract The paper examines the effects of composite material properties on the nonlinear buckling response of irregular asymmetric composite structures through the analysis of asymmetric laminated beam-columns composed of an arbitrary number of different material layers. The nonlinear buckling behavior of the structures subjected to combined compression and bending is examined as a function of the number, orientation and stacking sequence of the layers that make up the laminate. The analysis demonstrates that, typically, buckling of asymmetric composites is initiated immediately at the load a
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Nandi, Soumitra, Zahed Siddique, and M. Cengiz Altan. "A Grammatical Approach for Customization of Laminated Composite Materials." In ASME 2010 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/detc2010-28589.

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The wide range of properties covered by the manufacturable fiber-matrix combinations of composite materials, along with their directional property characteristics, provides designers with material selection flexibility during designing composite material products. Meeting multiple property goals, however, complicates the design process as both the composite material selection and the component shape formation become complicated because the loading conditions and matrix calculations are needed to determine theoretical value of composite material properties. This paper presents a grammatical app
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SNYDER, ALEXANDER D., ZACHARY J. PHILLIPS, and JASON F. PATRICK. "SELF-HEALING OF WOVEN COMPOSITE LAMINATES VIA IN SITU THERMAL REMENDING." In Thirty-sixth Technical Conference. Destech Publications, Inc., 2021. http://dx.doi.org/10.12783/asc36/35785.

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Fiber-reinforced polymer composites are attractive structural materials due to their high specific strength/stiffness and excellent corrosion resistance. However, the lack of through-thickness reinforcement in laminated composites creates inherent susceptibility to fiber-matrix debonding, i.e., interlaminar delamination. This internal damage mode has proven difficult to detect and nearly impossible to repair via conventional methods, and therefore, remains a significant factor limiting the reliability of composite laminates in lightweight structures. Thus, novel approaches for mitigation (e.g.
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Naik, Tushar, and Zhong Hu. "Computer Simulation of Deep Drawing Process for a Laminated Composite Cup." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-41593.

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The anisotropic nature of laminated composites creates a unique opportunity and also a great challenge for tailoring their behavior during the forming processes according to the design requirements. In this work, design and simulation of a deep drawing process for fiber-reinforced laminated composites were conducted by using finite element analysis. The effects of the fiber orientation and stacking order on the deep drawing process were investigated based on the basic understanding of forming process of the isotropic aluminum alloy (Al-1100) and laminated composite material (Grilon RVZ-15H nyl
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Lund, Erik. "Buckling Topology Optimization of Laminated Multi-Material Composite Structures." In ASME 8th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2006. http://dx.doi.org/10.1115/esda2006-95753.

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The design problem of maximizing the buckling load factor of laminated multi-material composite shell structures is investigated using the so-called Discrete Material Optimization (DMO) approach. The design optimization method is based on ideas from multi-phase topology optimization where the material stiffness is computed as a weighted sum of candidate materials, thus making it possible to solve discrete optimization problems using gradient based techniques and mathematical programming. The potential of the DMO method to solve the combinatorial problem of proper choice of material and fiber o
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Chuang, Shui-Nan. "Probabilistic Analysis for the Mechanical Properties of Cross-Ply Fiber-Reinforced Composite Laminate." In ASME 2006 International Mechanical Engineering Congress and Exposition. ASMEDC, 2006. http://dx.doi.org/10.1115/imece2006-13060.

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A probabilistic micromechanics model had been developed for the unidirectional fiber-reinforced composite material design screening. In which, we used the predicted mechanical properties of IM-7 carbon fiber from the existing IM-7/5250-4 composite material system together with the observed 977-3 matrix mechanical properties to predict the probability density functions for the mechanical properties of IM-7/977-3 unidirectional composite. To include the material design in the structural design process, we had extended the probabilistic analysis to predict the probability density functions for th
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Christoph, Jake E., Colin M. Gregg, Jordan R. Raney, and David A. Jack. "Low Velocity Impact Testing of Laminated Carbon Fiber/Carbon Nanotube Composites." In ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-52984.

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Carbon fiber laminated thermoset composites have become the industry standard for applications dictating a high strength-to-weight ratio. However, the brittle nature of the carbon fiber composite structure limits its energy dissipation characteristics, often leading to catastrophic failure under low energy impact loadings. This research examines the potential effects of including vertically aligned multi-walled carbon nanotube forests within a layered laminate structure with the goal being to increase the energy dissipation of the structure with attention given to the increase in the aerial de
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Erbil, Emre, and Ramazan Karakuzu. "Sleeve Design for Clinching Process on Laminated Composite Structures." In 6th International Students Science Congress. Izmir International Guest Student Association, 2022. http://dx.doi.org/10.52460/issc.2022.042.

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The lightweight composite materials bring out several opportunities besides some challenges. One of the most important challenges is to provide a strong and reliable joint for sensitive composite structures by preserving their specifications without any damage. Conventional fasteners are mostly designed for sheet metals, such as rivets, bolts, and clinched fixings are often incompatible with composites or require additional work. Moreover, interface materials may be required for additional functions like shock-absorbing, sealing, etc. For instance, a rivet can damage fiber or matrix during the
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Reports on the topic "Laminated composite material"

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Spera, D. A., J. B. Esgar, M. Gougeon, and M. D. Zuteck. Structural properties of laminated Douglas fir/epoxy composite material. Office of Scientific and Technical Information (OSTI), 1990. http://dx.doi.org/10.2172/6492500.

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Groves, S. E. Preliminary evaluation of the strength of pin-joints in laminated composite materials. Office of Scientific and Technical Information (OSTI), 1989. http://dx.doi.org/10.2172/7072288.

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Alexander, A., J. T. Tzeng, W. H. Drysdale, and B. P. Burns. Effective Three-Dimensional (3-D) Finite Element Material Stiffness Formulation for Modeling Laminated Composites. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada306454.

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