Добірка наукової літератури з теми "Laminated and sandwich composite"
Оформте джерело за APA, MLA, Chicago, Harvard та іншими стилями
Ознайомтеся зі списками актуальних статей, книг, дисертацій, тез та інших наукових джерел на тему "Laminated and sandwich composite".
Біля кожної праці в переліку літератури доступна кнопка «Додати до бібліографії». Скористайтеся нею – і ми автоматично оформимо бібліографічне посилання на обрану працю в потрібному вам стилі цитування: APA, MLA, «Гарвард», «Чикаго», «Ванкувер» тощо.
Також ви можете завантажити повний текст наукової публікації у форматі «.pdf» та прочитати онлайн анотацію до роботи, якщо відповідні параметри наявні в метаданих.
Статті в журналах з теми "Laminated and sandwich composite"
Sebaey, TA, and Ahmed Wagih. "Flexural properties of notched carbon–aramid hybrid composite laminates." Journal of Composite Materials 53, no. 28-30 (June 11, 2019): 4137–48. http://dx.doi.org/10.1177/0021998319855773.
Повний текст джерелаÇınar, Okan, Merve Erdal, and 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 (August 3, 2016): 139–66. http://dx.doi.org/10.1177/1099636215613934.
Повний текст джерелаLu, Ping, Xu Dong Liu, Xue Qiang Ma, and Wei Bo Huang. "Analysis of Damping Characteristics for Sandwich Beams with a Polyurea Viscoelastic Layer." Advanced Materials Research 374-377 (October 2011): 764–69. http://dx.doi.org/10.4028/www.scientific.net/amr.374-377.764.
Повний текст джерелаZhu, Xiujie, Chao Xiong, Junhui Yin, Dejun Yin, and Huiyong Deng. "Bending Experiment and Mechanical Properties Analysis of Composite Sandwich Laminated Box Beams." Materials 12, no. 18 (September 12, 2019): 2959. http://dx.doi.org/10.3390/ma12182959.
Повний текст джерелаHami, B., A. Irekti, C. Aribi, B. Bezzazi, and A. Mir. "Experimental Study of Sandwich Multilayer Reinforced by Glass Fibre and Agglomerated Cork." Advanced Composites Letters 23, no. 5 (September 2014): 096369351402300. http://dx.doi.org/10.1177/096369351402300503.
Повний текст джерелаCui, Xiao Dong, Tao Zeng, and Dai Ning Fang. "Study on Ballistic Energy Absorption of Laminated and Sandwich Composites." Key Engineering Materials 306-308 (March 2006): 739–44. http://dx.doi.org/10.4028/www.scientific.net/kem.306-308.739.
Повний текст джерелаBir, Amarpreet S., Hsin Piao Chen, and Hsun Hu Chen. "Optimum Stacking Sequence Design of Composite Sandwich Panel Using Genetic Algorithms." Advanced Materials Research 585 (November 2012): 29–33. http://dx.doi.org/10.4028/www.scientific.net/amr.585.29.
Повний текст джерелаVemuluri, Ramesh Babu, Vasudevan Rajamohan, and Ananda Babu Arumugam. "Dynamic characterization of tapered laminated composite sandwich plates partially treated with magnetorheological elastomer." Journal of Sandwich Structures & Materials 20, no. 3 (June 3, 2016): 308–50. http://dx.doi.org/10.1177/1099636216652573.
Повний текст джерелаKumar, Pavan, and CV Srinivasa. "On buckling and free vibration studies of sandwich plates and cylindrical shells: A review." Journal of Thermoplastic Composite Materials 33, no. 5 (November 11, 2018): 673–724. http://dx.doi.org/10.1177/0892705718809810.
Повний текст джерелаZenkour, AM, and 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 (June 12, 2016): 169–90. http://dx.doi.org/10.1177/1099636216644863.
Повний текст джерелаДисертації з теми "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.
Повний текст джерелаNayak, 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/.
Повний текст джерелаKilic, 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.
Повний текст джерелаIncludes 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, and 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.
Повний текст джерелаIn 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.
Повний текст джерелаGhinet, 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.
Повний текст джерелаShah, 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.
Повний текст джерелаPh. 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.
Повний текст джерелаDoctor 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.
Повний текст джерелаPh. 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.
Повний текст джерелаКниги з теми "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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаF, Lung S., Gupta K. K, and 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.
Знайти повний текст джерелаF, Lung S., Gupta K. K, and 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.
Знайти повний текст джерелаChamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаYu, 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.
Знайти повний текст джерелаMartin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.
Знайти повний текст джерелаR, Tullos Thomas, ed. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A: Noyes Publications, 1992.
Знайти повний текст джерелаVibrations of elastic plates: Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York: Springer, 1996.
Знайти повний текст джерелаNettles, A. T. (Alan T.), Jackson J. R, and 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.
Знайти повний текст джерелаЧастини книг з теми "Laminated and sandwich composite"
Vaidya, Uday K. "Impact Response of Laminated and Sandwich Composites." In Impact Engineering of Composite Structures, 97–191. Vienna: Springer Vienna, 2011. http://dx.doi.org/10.1007/978-3-7091-0523-8_4.
Повний текст джерелаManalo, Allan, Thiru Aravinthan, and Warna Karunasena. "Shear Behavior of Glue-Laminated Composite Sandwich Beams." In 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.
Повний текст джерелаDey, Sudip, Tanmoy Mukhopadhyay, and Sondipon Adhikari. "Uncertainty Quantification for Skewed Laminated Soft-core Sandwich Panels." In 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.
Повний текст джерелаKerr-Anderson, Eric, Selvum Pillay, Basir Shafiq, and Uday K. Vaidya. "Compressively Pre-stressed Navy Relevant Laminated and Sandwich Composites Subjected to Ballistic Impact." In 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.
Повний текст джерелаAltenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. "Elastic Behavior of Laminate and Sandwich Composites." In 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.
Повний текст джерелаAltenbach, Holm, Johannes Altenbach, and Wolfgang Kissing. "Elastic Behavior of Laminate and Sandwich Composites." In Mechanics of Composite Structural Elements, 103–76. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8935-0_4.
Повний текст джерелаZhu, Shengqing, and Gin Boay Chai. "Impact of Aluminum, CFRP Laminates, Fibre-Metal Laminates and Sandwich Panels." In 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.
Повний текст джерелаBaier, H. J. "Composite Laminate and Sandwich Optimization with Applications." In Optimization of Large Structural Systems, 997–1009. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-010-9577-8_51.
Повний текст джерелаJonna, Naresh, and J. Srinivas. "Aeroelastic Instability Characterization of Magnetorheological Fluid Filled-Core Laminated Composite Sandwich Beams." In Lecture Notes in Mechanical Engineering, 63–72. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2188-9_6.
Повний текст джерелаGarcía-Castillo, Shirley Kalamis, Sonia Sánchez-Sáez, Carlos Santiuste, Carlos Navarro, and Enrique Barbero. "Perforation of Composite Laminate Subjected to Dynamic Loads." In 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.
Повний текст джерелаТези доповідей конференцій з теми "Laminated and sandwich composite"
Dvorak, George J., Jian Zhang, and Olcay Canyurt. "Adhesive Joints for Composite Sandwich Structures." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2034.
Повний текст джерелаKatariya, Pankaj, and Subrata Kumar Panda. "Simulation Study of Transient Responses of Laminated Composite Sandwich Plate." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4846.
Повний текст джерелаAraújo, A. L., C. M. Mota Soares, C. A. Mota Soares, J. Herskovits, Jane W. Z. Lu, Andrew Y. T. Leung, Vai Pan Iu, and Kai Meng Mok. "Parameter Estimation in Hybrid Active-Passive Laminated Sandwich Composite Structures." In 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.
Повний текст джерелаDiveyev, Bohdan M., Ihor B. Butyter, and Natalie N. Shcherbyna. "High Order Theories for Elastic Modules Identification of Composite Plates." In ASME 2008 9th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2008. http://dx.doi.org/10.1115/esda2008-59278.
Повний текст джерелаVaidya, Uday K., Anthony N. Palazatto, and L. N. B. Gummadi. "Low Velocity Impact Response and Nondestructive Evaluation of Sandwich Composite Structures." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1045.
Повний текст джерелаWang, C. M., K. K. Ang, and C. Wang. "Vibration of Skew Sandwich Plates With Laminated Facings." In ASME 1997 Turbo Asia Conference. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-aa-050.
Повний текст джерелаBirman, Victor, and Larry W. Byrd. "On the Prediction of Damping in Composite and Sandwich Structures." In ASME 2001 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/imece2001/amd-25409.
Повний текст джерелаAlbernaz, Jessica. "Bending Analysis of Laminated Composite Sandwich Plates Reinforced with Carbon Nanotube Forests." In 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.
Повний текст джерелаKallannavar, Vinayak, and Subhaschandra Kattimani. "Modal analysis of laminated composite and sandwich plates using finite element method." In 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.
Повний текст джерелаGantovnik, Vladimir, Zafer Gurdal, and Layne Watson. "A Genetic Algorithm with Memory for Optimal Design of Laminated Sandwich Composite Panels." In 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.
Повний текст джерелаЗвіти організацій з теми "Laminated and sandwich composite"
Folias, E. S. Failure in Laminated Composite Plates Containing a Hole. Fort Belvoir, VA: Defense Technical Information Center, July 1990. http://dx.doi.org/10.21236/ada227307.
Повний текст джерелаSpera, 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), May 1990. http://dx.doi.org/10.2172/6492500.
Повний текст джерелаBarton, Oscar, Ratcliffe Jr., and Colin P. Fundamental Frequency of a Composite Sandwich Plate Containing Woven Layers. Fort Belvoir, VA: Defense Technical Information Center, August 1997. http://dx.doi.org/10.21236/ada359126.
Повний текст джерелаReddy, J. N. A Refined Nonlinear Analysis of Laminated Composite Plates and Shells. Fort Belvoir, VA: Defense Technical Information Center, August 1987. http://dx.doi.org/10.21236/ada184436.
Повний текст джерелаBlake, H. W., and J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), March 1993. http://dx.doi.org/10.2172/10151163.
Повний текст джерелаHammerand, Daniel Carl. Critical time step for a bilinear laminated composite Mindlin shell element. Office of Scientific and Technical Information (OSTI), June 2004. http://dx.doi.org/10.2172/919205.
Повний текст джерелаSandhu, R. S., W. E. Wolfe, R. L. Sierakowski, C. C. Chang, and H. R. Chu. Finite Element Analysis of Free-Edge Delamination in Laminated Composite Specimens. Fort Belvoir, VA: Defense Technical Information Center, June 1991. http://dx.doi.org/10.21236/ada251659.
Повний текст джерелаBlake, H. W., and J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), March 1993. http://dx.doi.org/10.2172/6855310.
Повний текст джерелаStephens, Max. Numerical and Experimental Analysis of Composite Sandwich Links for the LCF System. Portland State University Library, January 2000. http://dx.doi.org/10.15760/etd.579.
Повний текст джерелаGroves, S. E. Preliminary evaluation of the strength of pin-joints in laminated composite materials. Office of Scientific and Technical Information (OSTI), March 1989. http://dx.doi.org/10.2172/7072288.
Повний текст джерела