Academic literature on the topic 'Refined Zigzag Theory'
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Journal articles on the topic "Refined Zigzag Theory"
Iurlaro, Luigi, Marco Gherlone, Massimiliano Mattone, and Marco Di Sciuva. "Experimental assessment of the Refined Zigzag Theory for the static bending analysis of sandwich beams." Journal of Sandwich Structures & Materials 20, no. 1 (June 12, 2016): 86–105. http://dx.doi.org/10.1177/1099636216650614.
Full textTessler, Alexander, Marco Di Sciuva, and Marco Gherlone. "A Refined Zigzag Beam Theory for Composite and Sandwich Beams." Journal of Composite Materials 43, no. 9 (January 29, 2009): 1051–81. http://dx.doi.org/10.1177/0021998308097730.
Full textGhorbanpour-Arani, A., F. Kolahdouzan, and M. Abdollahian. "Nonlocal buckling of embedded magnetoelectroelastic sandwich nanoplate using refined zigzag theory." Applied Mathematics and Mechanics 39, no. 4 (February 20, 2018): 529–46. http://dx.doi.org/10.1007/s10483-018-2319-8.
Full textWimmer, Heinz, Werner Hochhauser, and Karin Nachbagauer. "Refined Zigzag Theory: an appropriate tool for the analysis of CLT-plates and other shear-elastic timber structures." European Journal of Wood and Wood Products 78, no. 6 (August 28, 2020): 1125–35. http://dx.doi.org/10.1007/s00107-020-01586-x.
Full textFlores, Fernando G., Sergio Oller, and Liz G. Nallim. "On the analysis of non-homogeneous laminates using the refined zigzag theory." Composite Structures 204 (November 2018): 791–802. http://dx.doi.org/10.1016/j.compstruct.2018.08.018.
Full textAscione, Alessia, and Marco Gherlone. "Nonlinear static response analysis of sandwich beams using the Refined Zigzag Theory." Journal of Sandwich Structures & Materials 22, no. 7 (August 23, 2018): 2250–86. http://dx.doi.org/10.1177/1099636218795381.
Full textTreviso, Alessandra, Domenico Mundo, and Michel Tournour. "Dynamic response of laminated structures using a Refined Zigzag Theory shell element." Composite Structures 159 (January 2017): 197–205. http://dx.doi.org/10.1016/j.compstruct.2016.09.026.
Full textHasim, K. Ahmet. "Isogeometric static analysis of laminated composite plane beams by using refined zigzag theory." Composite Structures 186 (February 2018): 365–74. http://dx.doi.org/10.1016/j.compstruct.2017.12.033.
Full textGherlone, Marco, Daniele Versino, and Vincenzo Zarra. "Multilayered triangular and quadrilateral flat shell elements based on the Refined Zigzag Theory." Composite Structures 233 (February 2020): 111629. http://dx.doi.org/10.1016/j.compstruct.2019.111629.
Full textNallim, Liz G., Sergio Oller, Eugenio Oñate, and Fernando G. Flores. "A hierarchical finite element for composite laminated beams using a refined zigzag theory." Composite Structures 163 (March 2017): 168–84. http://dx.doi.org/10.1016/j.compstruct.2016.12.031.
Full textDissertations / Theses on the topic "Refined Zigzag Theory"
Eijo, A. (Ariel). "Finite element modeling of delamination in advanced composite beams and plates using one- and two-dimensional finite elements based on the refined zigzag theory." Doctoral thesis, Universitat Politècnica de Catalunya, 2014. http://hdl.handle.net/10803/286739.
Full textAunque los materiales laminados se han utilizado durante décadas, su uso ha aumentado en los últimos años como resultado de una mayor confianza por parte de la industria. Esto ha proporcionado a la comunidad científica muchas razones para dedicar una considerable cantidad de tiempo y esfuerzos en aras de una mejor comprensión de su comportamiento mecánico. Con este objetivo tanto la simulación experimental como numérica han estado trabajando juntos para dar respuesta a una variedad de problemas relacionados con estos materiales. En cuanto a la simulación numérica, un correcto modelado de la cinemática de los materiales laminados es esencial para capturar el comportamiento real de la estructura. Por otra parte, una vez que la cinemática de la estructura se ha predicho con precisión otros fenómenos no lineales como los proceso de daño y/o plasticidad podrían ser también estudiados. En consecuencia, con el fin de contribuir al constante desarrollo de herramientas numéricas más simples y eficaces para modelar materiales laminados, un método numérico para el modelado de la delaminación (modo II/III) en materiales compuestos avanzados utilizando elementos finitos de una y dos dimensiones es propuesto en este trabajo. Además, dos elementos finitos para la simulación de vigas y placas de varias capas altamente heterogéneos son desarrollados aquí. El documento está escrito en base a los resultados de cuatro artículos publicados en revistas indexadas. Copias de estos artículos se incluyen en el Apéndice. El cuerpo principal de esta tesis está constituido por los Capítulos 2-4. El Capítulo 2 aborda el tratamiento numérico de vigas y placas laminadas. El capítulo 3 presenta la formulación de los elementos finitos de viga LRZ y placa QLRZ basados en la Teoría Zigzag Refinada. Finalmente, la principal contribución de esta tesis, el modelo de delaminación LRZ/QLRZ, se desarrolla en el capítulo 4.
Wei-LianDai and 戴維廉. "Applications of the Refined Zigzag Theorem (RZT) to exact solutions of cracked-sandwich-beam and composite beam with functionally graded materials." Thesis, 2019. http://ndltd.ncl.edu.tw/handle/xttj3e.
Full text國立成功大學
機械工程學系
107
In this thesis, the refined zigzag theory is used to solve the deflections and stresses of composite sandwich beam. According to the configurations of the sandwich beam, two parts are included in this study. In the first part, the cracked sandwich beam (CSB) is investigated by using the Refined Zigzag Theory (RZT). To solve the displacements, stresses, compliance and energy release reates, the continuity conditions at the crack tip and the boundary conditions are derived. By comparing the results between the theroretical predictions and finite element computations, the solutions by RZT are more accurate than those by FSDT (First-order Shear Deformation Theory). In the present study, parameters such as elastic modulus, shear modulus, layer thickness are considered to investigate their effects on the energy release rates of the CSB. In the second part, the RZT is extended to investigated the sandwich beam with functionally graded material. Various boundary conditions, loading conditions and spacial distribution models are considered to investigated their effects on the FGM sandwich beam. It reveals that the solutions by RZT agree very much with those by FEM and has low computational resources. Material properties equation in thickness direction and the effect of isotropic or orthotropic materials. In general, FGM is an isotropic material. Although FGM with orthotropic material has not developed on the market, it is expected that the numerical simulation results for FGM with orthotropic material presented of this paper will be applied to this new material in the future.
Book chapters on the topic "Refined Zigzag Theory"
Kefal, A., and A. Tessler. "Delamination damage identification in composite shell structures based on Inverse Finite Element Method and Refined Zigzag Theory." In Developments in the Analysis and Design of Marine Structures, 354–63. London: CRC Press, 2021. http://dx.doi.org/10.1201/9781003230373-41.
Full textKöpple, M., and W. Wagner. "A mixed refined zigzag theory for the modeling of layered plate structures." In Shell Structures: Theory and Applications Volume 4, 375–78. CRC Press, 2017. http://dx.doi.org/10.1201/9781315166605-85.
Full textConference papers on the topic "Refined Zigzag Theory"
Madenci, Erdogan, Mehmet Dorduncu, Atila Barut, and Nam D. Phan. "Progressive Failure Analysis of Composites Based on Peridynamics and Refined Zigzag Theory." In AIAA Scitech 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-1039.
Full textBarut, Atila, Erdogan Madenci, and Alexander Tessler. "A Refined Zigzag Theory for Laminated Composite and Sandwich Plates Incorporating Thickness Stretch Deformation." In 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.