Littérature scientifique sur le sujet « Laminated composite and sandwich plates and shell »
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Articles de revues sur le sujet "Laminated composite and sandwich plates and shell"
Kumar, 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 intégralDong, S. B., et C. K. Chun. « Shear Constitutive Relations for Laminated Anisotropic Shells and Plates : Part I—Methodology ». Journal of Applied Mechanics 59, no 2 (1 juin 1992) : 372–79. http://dx.doi.org/10.1115/1.2899530.
Texte intégralBrischetto, Salvatore. « Analysis of natural fibre composites for aerospace structures ». Aircraft Engineering and Aerospace Technology 90, no 9 (14 novembre 2018) : 1372–84. http://dx.doi.org/10.1108/aeat-06-2017-0152.
Texte intégralChun, C. K., et S. B. Dong. « Shear Constitutive Relations for Laminated Anisotropic Shells and Plates : Part II—Vibrations of Composite Cylinders ». Journal of Applied Mechanics 59, no 2 (1 juin 1992) : 380–89. http://dx.doi.org/10.1115/1.2899531.
Texte intégralLibrescu, L., W. Lin, M. DiSciuva et U. Icardi. « Postbuckling of laminated composite and sandwich plates and shells : On the significance of the fulfillment of static interlayer continuity conditions ». Computer Methods in Applied Mechanics and Engineering 148, no 1-2 (août 1997) : 165–86. http://dx.doi.org/10.1016/s0045-7825(97)00020-0.
Texte intégralMantari, J. L., A. S. Oktem et C. Guedes Soares. « Static and dynamic analysis of laminated composite and sandwich plates and shells by using a new higher-order shear deformation theory ». Composite Structures 94, no 1 (décembre 2011) : 37–49. http://dx.doi.org/10.1016/j.compstruct.2011.07.020.
Texte intégralSandeep, S. H., et C. V. Srinivasa. « Hybrid Sandwich Panels : A Review ». International Journal of Applied Mechanics and Engineering 25, no 3 (1 septembre 2020) : 64–85. http://dx.doi.org/10.2478/ijame-2020-0035.
Texte intégralKim, Chun-Gon, et Eui-Jin Jun. « Impact Resistance of Composite Laminated Sandwich Plates ». Journal of Composite Materials 26, no 15 (décembre 1992) : 2247–61. http://dx.doi.org/10.1177/002199839202601504.
Texte intégralMuc, Aleksander, Justyna Flis et Marcin Augustyn. « Optimal Design of Plated/Shell Structures under Flutter Constraints—A Literature Review ». Materials 12, no 24 (15 décembre 2019) : 4215. http://dx.doi.org/10.3390/ma12244215.
Texte intégralAnish et Ajay Kumar. « Ultimate Strength Analysis of Laminated Composite Sandwich Plates ». Structures 14 (juin 2018) : 95–110. http://dx.doi.org/10.1016/j.istruc.2018.02.004.
Texte intégralThèses sur le sujet "Laminated composite and sandwich plates and shell"
Nayak, 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 intégralMonge, 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
Liu, Chorng-Fuh. « Geometrically nonlinear analysis of composite laminates using a refined shear deformation shell theory ». Diss., Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/54453.
Texte intégralPh. D.
Chao, Ting-Mao, et 趙庭懋. « Mechanical Behavior of Laminated Composite Sandwich Plates ». Thesis, 1996. http://ndltd.ncl.edu.tw/handle/29336414269156617733.
Texte intégralChan, Tung-An, et 詹東恩. « Vibration and Sound Radiation of Laminated Composite Sandwich Plates ». Thesis, 2003. http://ndltd.ncl.edu.tw/handle/24918386418951555711.
Texte intégral國立交通大學
機械工程系
91
In this thesis, vibration characteristics of laminated composite sandwich plates are studied via experimental and theoretical approaches. Sound pressure responses of laminated composite sandwich plates with different vibration characteristics are also studied experimentally and theoretically. In the theoretical study, the vibration analysis of laminated composite sandwich plates is achieved via the use of the Rayliegh-Ritz Method. In sound pressure analysis, the modal and harmonic analyses of laminated plates are performed using the finite element code ANSYS. The amplitude and phase angle obtained from the harmonic analysis together with sound pressure equation are used to construct the sound pressure level (SPL) curves. The SPL curves change for different sizes of laminated composite sandwich plates in the sound pressure analysis. In the experiment approach, above all, the measured natural frequencies of laminated composite sandwich plates are used to verify the theoretical results. Furthermore, sound pressure responses of different sandwich plates are measured and used to verify the theoretical results. The comparison between the experimental and theoretical results shows that the present method can produce satisfactory results for both natural frequencies and SPL curves.
Yang, Tz-Ya, et 楊慈雅. « Impact Analysis and Experiment of Laminated Composite Sandwich Plates ». Thesis, 1997. http://ndltd.ncl.edu.tw/handle/38715647982356876130.
Texte intégral國立交通大學
機械工程研究所
85
A finite element method, which is formulated on the basis of the layerwise linear displacement theory, is used to study the mechanical behavior of laminated composite sandwich plates subjected to impact. Two types of finite elements, namely, three-node isoparametric triangular finite element and nine-node plate element, in conjunciton with an empirical contact law derived from the statical indentation test of laminated composite sandwich plates are used for the theoretical investigation. The impace problem is solved via the use of Newmark''s integration scheme and Newton-Raphson method. The proposed method is then used to evaluate the contact force and strains of the plates during impact. A number of examples of laminated composite sandwich plates with different length-to-thickness ratios, fiber angles and number of layer groups striked by an impactor with different velocities are studied. Results obtained via various theories are compared with experimental results. The suitability and accuracy of the proposed method are illustrated by means of the examples.
CHEN, WEN-JI, et 陳文吉. « Analysis of laminated composite plates and shell panels:vibration, buckling, and thermal buckling ». Thesis, 1992. http://ndltd.ncl.edu.tw/handle/43436673787665819682.
Texte intégralVeenaranjini, S. M. « Low-Order Laminated Lock-Free Beam And Plate Elements Based On Coupled Displacement Field ». Thesis, 2004. http://hdl.handle.net/2005/313.
Texte intégralLivres sur le sujet "Laminated composite and sandwich plates and shell"
F, 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 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 intégralVibrations of elastic plates : Linear and nonlinear dynamical modeling of sandwiches, laminated composites, and piezoelectric layers. New York : Springer, 1996.
Trouver le texte intégralVibrations of Elastic Plates : Linear and Nonlinear Dynamical Modeling of Sandwiches, Laminated Composites, and Piezoelectric Layers. Springer, 2011.
Trouver le texte intégralChapitres de livres sur le sujet "Laminated composite and sandwich plates and shell"
Kulikov, Gennady M., et Svetlana V. Plotnikova. « Three-Dimensional Exact Analysis of Functionally Graded Laminated Composite Plates ». Dans Shell and Membrane Theories in Mechanics and Biology, 223–41. Cham : Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-02535-3_13.
Texte intégral« Part 13 : Plates, shells, laminated composite structures, sandwich structures ». Dans Research and Applications in Structural Engineering, Mechanics and Computation, 349–50. CRC Press, 2013. http://dx.doi.org/10.1201/b15963-162.
Texte intégral« Plates, shells, pipes, laminated composites, sandwich structures ». Dans Advances and Trends in Structural Engineering, Mechanics and Computation. CRC Press, 2010. http://dx.doi.org/10.1201/b10557-8.
Texte intégral« A new trigonometric shear deformation theory for sandwich and composite laminated plates ». Dans Maritime Engineering and Technology, 331–36. CRC Press, 2012. http://dx.doi.org/10.1201/b12726-48.
Texte intégralActes de conférences sur le sujet "Laminated composite and sandwich plates and shell"
Katariya, 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 intégralLibrescu, Liviu. « Implication of Anisotropy of Face-Sheets and Core Layer Materials on the Load Carrying Capacity of Advanced Sandwich Panels : Linear and Nonlinear Responses ». Dans ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2039.
Texte intégralDvorak, 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 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 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 intégralYU, YI-YUAN. « Dynamics and vibration of layered plates and shells - A perspective from sandwiches to laminated composites ». Dans 30th Structures, Structural Dynamics and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1419.
Texte intégralBarut, Atila, Erdogan Madenci et Alexander Tessler. « A Refined Zigzag Theory for Laminated Composite and Sandwich Plates Incorporating Thickness Stretch Deformation ». Dans 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
20th AIAA/ASME/AHS Adaptive Structures Conference
14th AIAA. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-1705.
Diveyev, 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 intégralCarminelli, Antonio, et Giuseppe Catania. « B-Spline Finite Element Formulation for Laminated Composite Shells ». Dans ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-67420.
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