Littérature scientifique sur le sujet « Laminated and sandwich composite »
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Articles de revues sur le sujet "Laminated and sandwich composite"
Sebaey, TA, et Ahmed Wagih. « Flexural properties of notched carbon–aramid hybrid composite laminates ». Journal of Composite Materials 53, no 28-30 (11 juin 2019) : 4137–48. http://dx.doi.org/10.1177/0021998319855773.
Texte intégralÇınar, Okan, Merve Erdal et Altan Kayran. « Accurate equivalent models of sandwich laminates with honeycomb core and composite face sheets via optimization involving modal behavior ». Journal of Sandwich Structures & ; Materials 19, no 2 (3 août 2016) : 139–66. http://dx.doi.org/10.1177/1099636215613934.
Texte intégralLu, Ping, Xu Dong Liu, Xue Qiang Ma et Wei Bo Huang. « Analysis of Damping Characteristics for Sandwich Beams with a Polyurea Viscoelastic Layer ». Advanced Materials Research 374-377 (octobre 2011) : 764–69. http://dx.doi.org/10.4028/www.scientific.net/amr.374-377.764.
Texte intégralZhu, Xiujie, Chao Xiong, Junhui Yin, Dejun Yin et Huiyong Deng. « Bending Experiment and Mechanical Properties Analysis of Composite Sandwich Laminated Box Beams ». Materials 12, no 18 (12 septembre 2019) : 2959. http://dx.doi.org/10.3390/ma12182959.
Texte intégralHami, B., A. Irekti, C. Aribi, B. Bezzazi et A. Mir. « Experimental Study of Sandwich Multilayer Reinforced by Glass Fibre and Agglomerated Cork ». Advanced Composites Letters 23, no 5 (septembre 2014) : 096369351402300. http://dx.doi.org/10.1177/096369351402300503.
Texte intégralCui, Xiao Dong, Tao Zeng et Dai Ning Fang. « Study on Ballistic Energy Absorption of Laminated and Sandwich Composites ». Key Engineering Materials 306-308 (mars 2006) : 739–44. http://dx.doi.org/10.4028/www.scientific.net/kem.306-308.739.
Texte intégralBir, Amarpreet S., Hsin Piao Chen et Hsun Hu Chen. « Optimum Stacking Sequence Design of Composite Sandwich Panel Using Genetic Algorithms ». Advanced Materials Research 585 (novembre 2012) : 29–33. http://dx.doi.org/10.4028/www.scientific.net/amr.585.29.
Texte intégralVemuluri, Ramesh Babu, Vasudevan Rajamohan et Ananda Babu Arumugam. « Dynamic characterization of tapered laminated composite sandwich plates partially treated with magnetorheological elastomer ». Journal of Sandwich Structures & ; Materials 20, no 3 (3 juin 2016) : 308–50. http://dx.doi.org/10.1177/1099636216652573.
Texte intégralKumar, Pavan, et CV Srinivasa. « On buckling and free vibration studies of sandwich plates and cylindrical shells : A review ». Journal of Thermoplastic Composite Materials 33, no 5 (11 novembre 2018) : 673–724. http://dx.doi.org/10.1177/0892705718809810.
Texte intégralZenkour, AM, et AF Radwan. « Free vibration analysis of multilayered composite and soft core sandwich plates resting on Winkler–Pasternak foundations ». Journal of Sandwich Structures & ; Materials 20, no 2 (12 juin 2016) : 169–90. http://dx.doi.org/10.1177/1099636216644863.
Texte intégralThèses sur le sujet "Laminated and sandwich composite"
Zhao, Huyue. « Stress Analysis of Tapered Sandwich Panels with Isotropic or Laminated Composite Facings ». Fogler Library, University of Maine, 2002. http://www.library.umaine.edu/theses/pdf/ZhaoH2002.pdf.
Texte intégralNayak, Ajaya Kumar. « On dynamic analysis of laminated composite and sandwich plates using finite element method ». Thesis, University of Southampton, 2002. https://eprints.soton.ac.uk/43633/.
Texte intégralKilic, Yavuz S. M. Massachusetts Institute of Technology. « Impact and energy absorption of laminated and sandwich composites ». Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/44883.
Texte intégralIncludes bibliographical references (p. 115-131).
Advanced fiber reinforced composites combine high specific strength and stiffness. Advanced composites are currently being introduced into modern U.S. Navy ships to achieve weight savings, maintenance reduction, and signature reduction. These advancements manifest themselves in Naval ships as increases in survivability, payload, range, speed, and weapon systems performance. In this thesis, vinyl ester resin matrix laminates and sandwich composites are emphasized since they are increasingly being used in naval applications. Impact damage of laminated and sandwich composites under low-velocity and high-velocity impact are investigated. Delamination damage is explored in detail since delamination is one of the major failure modes of many advanced composites structures. Delamination initiation loads for various laminates having different stacking sequences are compared. In many laminates containing various stacking sequences, placing the 900 laminae on the outside (as opposed to the inside) will reduce the delamination initiation load under impact. Moreover, an open literature survey of numerous laminated and sandwich composites having different stacking sequences and thicknesses and subjected to low-velocity impact is undertaken. The failure mode, failure load, and displacement at failure of these composites are summarized. Other topics investigated include (1) effects of a composite's constituents on damage susceptibility, (2) post-impact residual characterization and strength, and (3) nondestructive testing techniques. Prediction methods for residual strength are tabulated based on the impact damage type for laminated and sandwich composites. Further, NASA and Boeing compression-after-impact tests are summarized for laminated composites after low-energy impacts.
(cont.) Damage and residual strength are analyzed for epoxy and PEEK resin laminates. An initial sorting for the selection of nondestructive testing methods for specific composite discontinuities is summarized. Extensive presentations of tables and figures are used to summarize the results of the literature surveys on impact resistance and energy absorbing capabilities of composites. Particular attention is given to methods for impact resistance improvement. Impact resistance improvement methods are compared according to increases in interlaminar Mode I and Mode II fracture toughness and in residual strength. These comparisons support data for the selection of impact resistance improvement. Numerous laminates having different lamina orientations are compared to understand the influence of stacking sequence on impact damage resistance and energy absorption capability. Matrix properties are investigated for many laminates and it is noted that higher interlaminar fracture toughness of matrix materials will increase energy absorption capability. The effects of other constituents of a laminate on impact resistance and energy absorbing capability are also summarized. Among the types of composites investigated in this thesis, carbon fiber/PEEK laminates exhibited the highest specific energy absorption. Recommendations for further studies are offered based on these summaries.
by Yavuz Kilic.
S.M.in Naval Architecture and Marine Engineering
Monge, J. C., J. L. Mantari et R. A. Arciniega. « Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells ». Elsevier Ltd, 2020. http://hdl.handle.net/10757/656405.
Texte intégralIn this paper, a three-dimensional numerical solution for the bending study of laminated composite doubly-curved shells is presented. The partial differential equations are solved analytically by the Navier summation for the midsurface variables; this method is only valid for shells with constant curvature where boundary conditions are considered simply supported. The partial differential equations present different coefficients, which depend on the thickness coordinates. A semi-analytical solution and the so-called Differential Quadrature Method are used to calculate an approximated derivative of a certain function by a weighted summation of the function evaluated in a certain grin domain. Each layer is discretized by a grid point distribution such as: Chebyshev-Gauss-Lobatto, Legendre, Ding and Uniform. As part of the formulation, the inter-laminar continuity conditions of displacements and transverse shear stresses between the interfaces of two layers are imposed. The proper traction conditions at the top and bottom of the shell due to applied transverse loadings are also considered. The present results are compared with other 3D solutions available in the literature, classical 2D models, Layer-wise models, etc. Comparison of the results show that the present formulation correctly predicts through-the-thickness distributions for stresses and displacements while maintaining a low computational cost.
Consejo Nacional de Ciencia, TecnologÃa e Innovación Tecnológica
Ghoor, Ismail B. « The response of concave singly curved fibre reinforced moulded sandwich and laminated composite panels to blast loading ». Master's thesis, University of Cape Town, 2018. http://hdl.handle.net/11427/27811.
Texte intégralGhinet, Sebastian. « Statistical energy analysis of the transmission loss of sandwich and laminate composite structures ». Thèse, Université de Sherbrooke, 2005. http://savoirs.usherbrooke.ca/handle/11143/1770.
Texte intégralShah, Priyal. « Computational Analysis of Elastic Moduli of Covalently Functionalized Carbon Nanomaterials, Infinitesimal Elastostatic Deformations of Doubly Curved Laminated Shells, and Curing of Laminates ». Diss., Virginia Tech, 2017. http://hdl.handle.net/10919/77034.
Texte intégralPh. D.
Alanbay, Berkan. « Free Vibrations and Static Deformations of Composite Laminates and Sandwich Plates using Ritz Method ». Diss., Virginia Tech, 2020. http://hdl.handle.net/10919/103087.
Texte intégralDoctor of Philosophy
In everyday life, plate-like structures find applications such as boards displaying advertisements, signs on shops and panels on automobiles. These structures are typically nailed, welded, or glued to supports at one or more edges. When subjected to disturbances such as wind gusts, plate-like structures vibrate. The frequency (number of cycles per second) of a structure in the absence of an applied external load is called its natural frequency that depends upon plate's geometric dimensions, its material and how it is supported at the edges. If the frequency of an applied disturbance matches one of the natural frequencies of the plate, then it will vibrate violently. To avoid such situations in structural designs, it is important to know the natural frequencies of a plate under different support conditions. One would also expect the plate to be able to support the designed structural load without breaking; hence knowledge of plate's deformations and stresses developed in it is equally important. These require mathematical models that adequately characterize their static and dynamic behavior. Most mathematical models are based on plate theories. Although plates are three-dimensional (3D) objects, their thickness is small as compared to the in-plane dimensions. Thus, they are analyzed as 2D objects using assumptions on the displacement fields and using quantities averaged over the plate thickness. These provide many plate theories, each with its own computational efficiency and fidelity (the degree to which it reproduces behavior of the 3-D object). Hence, a plate theory can be developed to provide accurately a quantity of interest. Some issues are more challenging for low-fidelity plate theories than others. For example, the greater the plate thickness, the higher the fidelity of plate theories required for obtaining accurate natural frequencies and deformations. Another challenging issue arises when a sandwich structure consists of strong face-sheets (e.g., made of carbon fiber-reinforced epoxy composite) and a soft core (e.g., made of foam) embedded between them. Sandwich structures exhibit more complex behavior than monolithic plates. Thus, many widely used plate theories may not provide accurate results for them. Here, we have used different plate theories to solve problems including those for sandwich structures. The governing equations of the plate theories are solved numerically (i.e., they are approximately satisfied) using the Ritz method named after Walter Ritz and weighted Jacobi polynomials. It is shown that these provide accurate solutions and the corresponding numerical algorithms are computationally more economical than the commonly used finite element method. To evaluate the accuracy of a plate theory, we have analytically solved (i.e., the governing equations are satisfied at every point in the problem domain) equations of the 3D theory of linear elasticity. The results presented in this research should help structural designers.
Taetragool, Unchalisa. « Optimal Parameters for Doubly Curved Sandwich Shells, Composite Laminates, and Atmospheric Plasma Spray Process ». Diss., Virginia Tech, 2018. http://hdl.handle.net/10919/81978.
Texte intégralPh. D.
Elmushyakhi, Abraham. « In-Plane Fatigue Characterization of Core Joints in Sandwich Composite Structures ». University of Dayton / OhioLINK, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1510678155755824.
Texte intégralLivres sur le sujet "Laminated and sandwich composite"
Center, Langley Research, dir. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.
Trouver le texte intégralCenter, Langley Research, dir. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.
Trouver le texte intégralF, Lung S., Gupta K. K et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. A three-node C ̊element for analysis of laminated composite sandwich shells. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Trouver le texte intégralF, Lung S., Gupta K. K et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. A three-node C ̊element for analysis of laminated composite sandwich shells. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Trouver le texte intégralChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC] : National Aeronautics and Space Administration, 1986.
Trouver le texte intégralYu, Yi-Yuan. Vibrations of Elastic Plates : Linear and Nonlinear Dynamical Modeling of Sandwiches, Laminated Composites, and Piezoelectric Layers. New York, NY : Springer New York, 1996.
Trouver le texte intégralMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif : Ames Research Center, 1989.
Trouver le texte intégralR, Tullos Thomas, dir. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A : Noyes Publications, 1992.
Trouver le texte intégralVibrations of elastic plates : Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York : Springer, 1996.
Trouver le texte intégralNettles, A. T. (Alan T.), Jackson J. R et George C. Marshall Space Flight Center, dir. Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage. Huntsville], Ala : National Aeronautics and Space Administration, Marshall Space Flight Center, 2011.
Trouver le texte intégralChapitres de livres sur le sujet "Laminated and sandwich composite"
Vaidya, Uday K. « Impact Response of Laminated and Sandwich Composites ». Dans Impact Engineering of Composite Structures, 97–191. Vienna : Springer Vienna, 2011. http://dx.doi.org/10.1007/978-3-7091-0523-8_4.
Texte intégralManalo, Allan, Thiru Aravinthan et Warna Karunasena. « Shear Behavior of Glue-Laminated Composite Sandwich Beams ». Dans Advances in FRP Composites in Civil Engineering, 139–43. Berlin, Heidelberg : Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-17487-2_29.
Texte intégralDey, Sudip, Tanmoy Mukhopadhyay et Sondipon Adhikari. « Uncertainty Quantification for Skewed Laminated Soft-core Sandwich Panels ». Dans Uncertainty Quantification in Laminated Composites, 220–49. Boca Raton, FL : CRC Press, Taylor & Francis Group, [2018] | “A science publishers book.” : CRC Press, 2018. http://dx.doi.org/10.1201/9781315155593-10.
Texte intégralKerr-Anderson, Eric, Selvum Pillay, Basir Shafiq et Uday K. Vaidya. « Compressively Pre-stressed Navy Relevant Laminated and Sandwich Composites Subjected to Ballistic Impact ». Dans Dynamic Failure of Composite and Sandwich Structures, 151–76. Dordrecht : Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5329-7_4.
Texte intégralAltenbach, Holm, Johannes Altenbach et Wolfgang Kissing. « Elastic Behavior of Laminate and Sandwich Composites ». Dans Mechanics of Composite Structural Elements, 91–160. Berlin, Heidelberg : Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08589-9_4.
Texte intégralAltenbach, Holm, Johannes Altenbach et Wolfgang Kissing. « Elastic Behavior of Laminate and Sandwich Composites ». Dans Mechanics of Composite Structural Elements, 103–76. Singapore : Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8935-0_4.
Texte intégralZhu, Shengqing, et Gin Boay Chai. « Impact of Aluminum, CFRP Laminates, Fibre-Metal Laminates and Sandwich Panels ». Dans Composite Materials and Joining Technologies for Composites, Volume 7, 199–205. New York, NY : Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-4553-1_21.
Texte intégralBaier, H. J. « Composite Laminate and Sandwich Optimization with Applications ». Dans Optimization of Large Structural Systems, 997–1009. Dordrecht : Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-010-9577-8_51.
Texte intégralJonna, Naresh, et J. Srinivas. « Aeroelastic Instability Characterization of Magnetorheological Fluid Filled-Core Laminated Composite Sandwich Beams ». Dans Lecture Notes in Mechanical Engineering, 63–72. Singapore : Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2188-9_6.
Texte intégralGarcía-Castillo, Shirley Kalamis, Sonia Sánchez-Sáez, Carlos Santiuste, Carlos Navarro et Enrique Barbero. « Perforation of Composite Laminate Subjected to Dynamic Loads ». Dans Dynamic Failure of Composite and Sandwich Structures, 291–337. Dordrecht : Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5329-7_7.
Texte intégralActes de conférences sur le sujet "Laminated and sandwich composite"
Dvorak, George J., Jian Zhang et Olcay Canyurt. « Adhesive Joints for Composite Sandwich Structures ». Dans ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2034.
Texte intégralKatariya, Pankaj, et Subrata Kumar Panda. « Simulation Study of Transient Responses of Laminated Composite Sandwich Plate ». Dans ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4846.
Texte intégralAraújo, A. L., C. M. Mota Soares, C. A. Mota Soares, J. Herskovits, Jane W. Z. Lu, Andrew Y. T. Leung, Vai Pan Iu et Kai Meng Mok. « Parameter Estimation in Hybrid Active-Passive Laminated Sandwich Composite Structures ». Dans PROCEEDINGS OF THE 2ND INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL MECHANICS AND THE 12TH INTERNATIONAL CONFERENCE ON THE ENHANCEMENT AND PROMOTION OF COMPUTATIONAL METHODS IN ENGINEERING AND SCIENCE. AIP, 2010. http://dx.doi.org/10.1063/1.3452037.
Texte intégralDiveyev, Bohdan M., Ihor B. Butyter et Natalie N. Shcherbyna. « High Order Theories for Elastic Modules Identification of Composite Plates ». Dans ASME 2008 9th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2008. http://dx.doi.org/10.1115/esda2008-59278.
Texte intégralVaidya, Uday K., Anthony N. Palazatto et L. N. B. Gummadi. « Low Velocity Impact Response and Nondestructive Evaluation of Sandwich Composite Structures ». Dans ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1045.
Texte intégralWang, C. M., K. K. Ang et C. Wang. « Vibration of Skew Sandwich Plates With Laminated Facings ». Dans ASME 1997 Turbo Asia Conference. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-aa-050.
Texte intégralBirman, Victor, et Larry W. Byrd. « On the Prediction of Damping in Composite and Sandwich Structures ». Dans ASME 2001 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/imece2001/amd-25409.
Texte intégralAlbernaz, Jessica. « Bending Analysis of Laminated Composite Sandwich Plates Reinforced with Carbon Nanotube Forests ». Dans 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-200.
Texte intégralKallannavar, Vinayak, et Subhaschandra Kattimani. « Modal analysis of laminated composite and sandwich plates using finite element method ». Dans ADVANCES IN MECHANICAL DESIGN, MATERIALS AND MANUFACTURE : Proceeding of the Second International Conference on Design, Materials and Manufacture (ICDEM 2019). AIP Publishing, 2020. http://dx.doi.org/10.1063/5.0004159.
Texte intégralGantovnik, Vladimir, Zafer Gurdal et Layne Watson. « A Genetic Algorithm with Memory for Optimal Design of Laminated Sandwich Composite Panels ». Dans 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-1221.
Texte intégralRapports d'organisations sur le sujet "Laminated and sandwich composite"
Folias, E. S. Failure in Laminated Composite Plates Containing a Hole. Fort Belvoir, VA : Defense Technical Information Center, juillet 1990. http://dx.doi.org/10.21236/ada227307.
Texte intégralSpera, D. A., J. B. Esgar, M. Gougeon et M. D. Zuteck. Structural properties of laminated Douglas fir/epoxy composite material. Office of Scientific and Technical Information (OSTI), mai 1990. http://dx.doi.org/10.2172/6492500.
Texte intégralBarton, Oscar, Ratcliffe Jr. et Colin P. Fundamental Frequency of a Composite Sandwich Plate Containing Woven Layers. Fort Belvoir, VA : Defense Technical Information Center, août 1997. http://dx.doi.org/10.21236/ada359126.
Texte intégralReddy, J. N. A Refined Nonlinear Analysis of Laminated Composite Plates and Shells. Fort Belvoir, VA : Defense Technical Information Center, août 1987. http://dx.doi.org/10.21236/ada184436.
Texte intégralBlake, H. W., et J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), mars 1993. http://dx.doi.org/10.2172/10151163.
Texte intégralHammerand, Daniel Carl. Critical time step for a bilinear laminated composite Mindlin shell element. Office of Scientific and Technical Information (OSTI), juin 2004. http://dx.doi.org/10.2172/919205.
Texte intégralSandhu, R. S., W. E. Wolfe, R. L. Sierakowski, C. C. Chang et H. R. Chu. Finite Element Analysis of Free-Edge Delamination in Laminated Composite Specimens. Fort Belvoir, VA : Defense Technical Information Center, juin 1991. http://dx.doi.org/10.21236/ada251659.
Texte intégralBlake, H. W., et J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), mars 1993. http://dx.doi.org/10.2172/6855310.
Texte intégralStephens, Max. Numerical and Experimental Analysis of Composite Sandwich Links for the LCF System. Portland State University Library, janvier 2000. http://dx.doi.org/10.15760/etd.579.
Texte intégralGroves, S. E. Preliminary evaluation of the strength of pin-joints in laminated composite materials. Office of Scientific and Technical Information (OSTI), mars 1989. http://dx.doi.org/10.2172/7072288.
Texte intégral