Literatura académica sobre el tema "Laminated and sandwich composite"
Crea una cita precisa en los estilos APA, MLA, Chicago, Harvard y otros
Consulte las listas temáticas de artículos, libros, tesis, actas de conferencias y otras fuentes académicas sobre el tema "Laminated and sandwich composite".
Junto a cada fuente en la lista de referencias hay un botón "Agregar a la bibliografía". Pulsa este botón, y generaremos automáticamente la referencia bibliográfica para la obra elegida en el estilo de cita que necesites: APA, MLA, Harvard, Vancouver, Chicago, etc.
También puede descargar el texto completo de la publicación académica en formato pdf y leer en línea su resumen siempre que esté disponible en los metadatos.
Artículos de revistas sobre el tema "Laminated and sandwich composite"
Sebaey, TA y Ahmed Wagih. "Flexural properties of notched carbon–aramid hybrid composite laminates". Journal of Composite Materials 53, n.º 28-30 (11 de junio de 2019): 4137–48. http://dx.doi.org/10.1177/0021998319855773.
Texto completoÇınar, Okan, Merve Erdal y 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, n.º 2 (3 de agosto de 2016): 139–66. http://dx.doi.org/10.1177/1099636215613934.
Texto completoLu, Ping, Xu Dong Liu, Xue Qiang Ma y Wei Bo Huang. "Analysis of Damping Characteristics for Sandwich Beams with a Polyurea Viscoelastic Layer". Advanced Materials Research 374-377 (octubre de 2011): 764–69. http://dx.doi.org/10.4028/www.scientific.net/amr.374-377.764.
Texto completoZhu, Xiujie, Chao Xiong, Junhui Yin, Dejun Yin y Huiyong Deng. "Bending Experiment and Mechanical Properties Analysis of Composite Sandwich Laminated Box Beams". Materials 12, n.º 18 (12 de septiembre de 2019): 2959. http://dx.doi.org/10.3390/ma12182959.
Texto completoHami, B., A. Irekti, C. Aribi, B. Bezzazi y A. Mir. "Experimental Study of Sandwich Multilayer Reinforced by Glass Fibre and Agglomerated Cork". Advanced Composites Letters 23, n.º 5 (septiembre de 2014): 096369351402300. http://dx.doi.org/10.1177/096369351402300503.
Texto completoCui, Xiao Dong, Tao Zeng y Dai Ning Fang. "Study on Ballistic Energy Absorption of Laminated and Sandwich Composites". Key Engineering Materials 306-308 (marzo de 2006): 739–44. http://dx.doi.org/10.4028/www.scientific.net/kem.306-308.739.
Texto completoBir, Amarpreet S., Hsin Piao Chen y Hsun Hu Chen. "Optimum Stacking Sequence Design of Composite Sandwich Panel Using Genetic Algorithms". Advanced Materials Research 585 (noviembre de 2012): 29–33. http://dx.doi.org/10.4028/www.scientific.net/amr.585.29.
Texto completoVemuluri, Ramesh Babu, Vasudevan Rajamohan y Ananda Babu Arumugam. "Dynamic characterization of tapered laminated composite sandwich plates partially treated with magnetorheological elastomer". Journal of Sandwich Structures & Materials 20, n.º 3 (3 de junio de 2016): 308–50. http://dx.doi.org/10.1177/1099636216652573.
Texto completoKumar, Pavan y CV Srinivasa. "On buckling and free vibration studies of sandwich plates and cylindrical shells: A review". Journal of Thermoplastic Composite Materials 33, n.º 5 (11 de noviembre de 2018): 673–724. http://dx.doi.org/10.1177/0892705718809810.
Texto completoZenkour, AM y AF Radwan. "Free vibration analysis of multilayered composite and soft core sandwich plates resting on Winkler–Pasternak foundations". Journal of Sandwich Structures & Materials 20, n.º 2 (12 de junio de 2016): 169–90. http://dx.doi.org/10.1177/1099636216644863.
Texto completoTesis sobre el tema "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.
Texto completoNayak, 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/.
Texto completoKilic, 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.
Texto completoIncludes 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 y 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.
Texto completoIn 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.
Texto completoGhinet, 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.
Texto completoShah, 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.
Texto completoPh. 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.
Texto completoDoctor 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.
Texto completoPh. 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.
Texto completoLibros sobre el tema "Laminated and sandwich composite"
Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Buscar texto completoCenter, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Buscar texto completoF, Lung S., Gupta K. K y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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.
Buscar texto completoF, Lung S., Gupta K. K y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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.
Buscar texto completoChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Buscar texto completoYu, 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.
Buscar texto completoMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.
Buscar texto completoR, Tullos Thomas, ed. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A: Noyes Publications, 1992.
Buscar texto completoVibrations of elastic plates: Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York: Springer, 1996.
Buscar texto completoNettles, A. T. (Alan T.), Jackson J. R y George C. Marshall Space Flight Center, eds. 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.
Buscar texto completoCapítulos de libros sobre el tema "Laminated and sandwich composite"
Vaidya, Uday K. "Impact Response of Laminated and Sandwich Composites". En Impact Engineering of Composite Structures, 97–191. Vienna: Springer Vienna, 2011. http://dx.doi.org/10.1007/978-3-7091-0523-8_4.
Texto completoManalo, Allan, Thiru Aravinthan y Warna Karunasena. "Shear Behavior of Glue-Laminated Composite Sandwich Beams". En 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.
Texto completoDey, Sudip, Tanmoy Mukhopadhyay y Sondipon Adhikari. "Uncertainty Quantification for Skewed Laminated Soft-core Sandwich Panels". En 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.
Texto completoKerr-Anderson, Eric, Selvum Pillay, Basir Shafiq y Uday K. Vaidya. "Compressively Pre-stressed Navy Relevant Laminated and Sandwich Composites Subjected to Ballistic Impact". En 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.
Texto completoAltenbach, Holm, Johannes Altenbach y Wolfgang Kissing. "Elastic Behavior of Laminate and Sandwich Composites". En 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.
Texto completoAltenbach, Holm, Johannes Altenbach y Wolfgang Kissing. "Elastic Behavior of Laminate and Sandwich Composites". En Mechanics of Composite Structural Elements, 103–76. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8935-0_4.
Texto completoZhu, Shengqing y Gin Boay Chai. "Impact of Aluminum, CFRP Laminates, Fibre-Metal Laminates and Sandwich Panels". En 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.
Texto completoBaier, H. J. "Composite Laminate and Sandwich Optimization with Applications". En Optimization of Large Structural Systems, 997–1009. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-010-9577-8_51.
Texto completoJonna, Naresh y J. Srinivas. "Aeroelastic Instability Characterization of Magnetorheological Fluid Filled-Core Laminated Composite Sandwich Beams". En Lecture Notes in Mechanical Engineering, 63–72. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2188-9_6.
Texto completoGarcía-Castillo, Shirley Kalamis, Sonia Sánchez-Sáez, Carlos Santiuste, Carlos Navarro y Enrique Barbero. "Perforation of Composite Laminate Subjected to Dynamic Loads". En 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.
Texto completoActas de conferencias sobre el tema "Laminated and sandwich composite"
Dvorak, George J., Jian Zhang y Olcay Canyurt. "Adhesive Joints for Composite Sandwich Structures". En ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2034.
Texto completoKatariya, Pankaj y Subrata Kumar Panda. "Simulation Study of Transient Responses of Laminated Composite Sandwich Plate". En ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4846.
Texto completoAraújo, A. L., C. M. Mota Soares, C. A. Mota Soares, J. Herskovits, Jane W. Z. Lu, Andrew Y. T. Leung, Vai Pan Iu y Kai Meng Mok. "Parameter Estimation in Hybrid Active-Passive Laminated Sandwich Composite Structures". En 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.
Texto completoDiveyev, Bohdan M., Ihor B. Butyter y Natalie N. Shcherbyna. "High Order Theories for Elastic Modules Identification of Composite Plates". En ASME 2008 9th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2008. http://dx.doi.org/10.1115/esda2008-59278.
Texto completoVaidya, Uday K., Anthony N. Palazatto y L. N. B. Gummadi. "Low Velocity Impact Response and Nondestructive Evaluation of Sandwich Composite Structures". En ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1045.
Texto completoWang, C. M., K. K. Ang y C. Wang. "Vibration of Skew Sandwich Plates With Laminated Facings". En ASME 1997 Turbo Asia Conference. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-aa-050.
Texto completoBirman, Victor y Larry W. Byrd. "On the Prediction of Damping in Composite and Sandwich Structures". En ASME 2001 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/imece2001/amd-25409.
Texto completoAlbernaz, Jessica. "Bending Analysis of Laminated Composite Sandwich Plates Reinforced with Carbon Nanotube Forests". En 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.
Texto completoKallannavar, Vinayak y Subhaschandra Kattimani. "Modal analysis of laminated composite and sandwich plates using finite element method". En 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.
Texto completoGantovnik, Vladimir, Zafer Gurdal y Layne Watson. "A Genetic Algorithm with Memory for Optimal Design of Laminated Sandwich Composite Panels". En 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.
Texto completoInformes sobre el tema "Laminated and sandwich composite"
Folias, E. S. Failure in Laminated Composite Plates Containing a Hole. Fort Belvoir, VA: Defense Technical Information Center, julio de 1990. http://dx.doi.org/10.21236/ada227307.
Texto completoSpera, D. A., J. B. Esgar, M. Gougeon y M. D. Zuteck. Structural properties of laminated Douglas fir/epoxy composite material. Office of Scientific and Technical Information (OSTI), mayo de 1990. http://dx.doi.org/10.2172/6492500.
Texto completoBarton, Oscar, Ratcliffe Jr. y Colin P. Fundamental Frequency of a Composite Sandwich Plate Containing Woven Layers. Fort Belvoir, VA: Defense Technical Information Center, agosto de 1997. http://dx.doi.org/10.21236/ada359126.
Texto completoReddy, J. N. A Refined Nonlinear Analysis of Laminated Composite Plates and Shells. Fort Belvoir, VA: Defense Technical Information Center, agosto de 1987. http://dx.doi.org/10.21236/ada184436.
Texto completoBlake, H. W. y J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), marzo de 1993. http://dx.doi.org/10.2172/10151163.
Texto completoHammerand, Daniel Carl. Critical time step for a bilinear laminated composite Mindlin shell element. Office of Scientific and Technical Information (OSTI), junio de 2004. http://dx.doi.org/10.2172/919205.
Texto completoSandhu, R. S., W. E. Wolfe, R. L. Sierakowski, C. C. Chang y H. R. Chu. Finite Element Analysis of Free-Edge Delamination in Laminated Composite Specimens. Fort Belvoir, VA: Defense Technical Information Center, junio de 1991. http://dx.doi.org/10.21236/ada251659.
Texto completoBlake, H. W. y J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), marzo de 1993. http://dx.doi.org/10.2172/6855310.
Texto completoStephens, Max. Numerical and Experimental Analysis of Composite Sandwich Links for the LCF System. Portland State University Library, enero de 2000. http://dx.doi.org/10.15760/etd.579.
Texto completoGroves, S. E. Preliminary evaluation of the strength of pin-joints in laminated composite materials. Office of Scientific and Technical Information (OSTI), marzo de 1989. http://dx.doi.org/10.2172/7072288.
Texto completo