Littérature scientifique sur le sujet « Laminate composite NCF »
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Articles de revues sur le sujet "Laminate composite NCF"
Monticeli, Francisco Maciel, David Daou, Mirko Dinulović, Herman Jacobus Cornelis Voorwald et Maria Odila Hilário Cioffi. « Mechanical behavior simulation : NCF/epoxy composite processed by RTM ». Polymers and Polymer Composites 27, no 2 (9 décembre 2018) : 66–75. http://dx.doi.org/10.1177/0967391118817174.
Texte intégralMitchell, Cynthia J., James A. Sherwood, Konstantine A. Fetfatsidis et Lisa M. Dangora. « Characterization of Cured Composite Materials for Wind Turbine Blades ». Key Engineering Materials 554-557 (juin 2013) : 478–83. http://dx.doi.org/10.4028/www.scientific.net/kem.554-557.478.
Texte intégralPapila, Melih. « Design of and with thin-ply non-crimp fabric as building blocks for composites ». Science and Engineering of Composite Materials 25, no 3 (25 avril 2018) : 501–16. http://dx.doi.org/10.1515/secm-2015-0386.
Texte intégralMohsin, Muhammad Ameerul Atrash, Lorenzo Iannucci et Emile S. Greenhalgh. « Delamination of Novel Carbon Fibre-Based Non-Crimp Fabric-Reinforced Thermoplastic Composites in Mode I : Experimental and Fractographic Analysis ». Polymers 15, no 7 (23 mars 2023) : 1611. http://dx.doi.org/10.3390/polym15071611.
Texte intégralMohsin, Muhammad Ameerul Atrash, Lorenzo Iannucci et Emile S. Greenhalgh. « Experimental and Numerical Analysis of Low-Velocity Impact of Carbon Fibre-Based Non-Crimp Fabric Reinforced Thermoplastic Composites ». Polymers 13, no 21 (22 octobre 2021) : 3642. http://dx.doi.org/10.3390/polym13213642.
Texte intégralKunze, Eckart, Siegfried Galkin, Robert Böhm, Maik Gude et Luise Kärger. « The Impact of Draping Effects on the Stiffness and Failure Behavior of Unidirectional Non-Crimp Fabric Fiber Reinforced Composites ». Materials 13, no 13 (2 juillet 2020) : 2959. http://dx.doi.org/10.3390/ma13132959.
Texte intégralİnal, Oğuzcan, Fatih Balıkoğlu et Akın Ataş. « Bolted joints in quasi-unidirectional glass-fibre NCF composite laminates ». Composite Structures 183 (janvier 2018) : 536–44. http://dx.doi.org/10.1016/j.compstruct.2017.05.075.
Texte intégralGovindasamy, Mahendran, Gopalakrishnan Kamalakannan, Chandrasekaran Kesavan et Ganesh Kumar Meenashisundaram. « Damage Detection in Glass/Epoxy Laminated Composite Plates Using Modal Curvature for Structural Health Monitoring Applications ». Journal of Composites Science 4, no 4 (14 décembre 2020) : 185. http://dx.doi.org/10.3390/jcs4040185.
Texte intégralByeon, Ki-Seok, Yu-Jeong Shin, Han-Kyu Jeung, Si-Woo Park, Chun-Su Roh, Jin-Soo Je et Ki-Chul Kwon. « Tensile Property Analysis of NCF Composite Laminated Structure for HP-CRTM Forming Process ». Korean Society of Manufacturing Process Engineers 18, no 1 (31 janvier 2019) : 59–64. http://dx.doi.org/10.14775/ksmpe.2019.18.1.059.
Texte intégralGrauers, L., R. Olsson et R. Gutkin. « Energy absorption and damage mechanisms in progressive crushing of corrugated NCF laminates : Fractographic analysis ». Composite Structures 110 (avril 2014) : 110–17. http://dx.doi.org/10.1016/j.compstruct.2013.11.001.
Texte intégralThèses sur le sujet "Laminate composite NCF"
Boukar, Ahmed. « Etude expérimentale et modélisation prédictive du comportement à l’impact des composites stratifiés ». Electronic Thesis or Diss., IMT Mines Alès, 2022. http://www.theses.fr/2022EMAL0015.
Texte intégralThis work consists of an experimental and numerical study of the behavior and strength of laminated composites subjected to a low velocity/low energy impact. The main objective is to develop a robust model capable of predicting the static and dynamic response of laminated composites, based on accurate experimental observations. Impact tests have been performed using a drop tower instrumented with high-speed cameras to monitor the evolution of damage in real time. The 3D finite element study of impact in explicit dynamics allows to judge the applicability of the failure criteria and the damage evolution methods. Various progressive damage models are implemented to predict the initiation and accumulation of damage in an NCF composite laminate. Cohesive elements are also inserted between adjacent plies to account for inter-ply delamination. In a second step, the model has been validated to reliably simulate the evolution of the mechanisms until failure, under quasi-static loading situations. In this case, the NCF composite is modeled using a unitary constitutive model at mesoscale, and presenting idealized regions of the polymer matrix and impregnated wicks. The idealized unitary model is defined on the basis of data from image analysis. The proposed methodology is generic, using a 3D elemental representation of the part for the global analysis, as well as the non-linearity of the matrix and the local response to the damage
Ben, Kahla Hiba. « Microfissures et délaminations des composites stratifiés soumis à des chargements quasi-statiques et cycliques ». Electronic Thesis or Diss., Université de Lorraine, 2019. http://www.theses.fr/2019LORR0333.
Texte intégralAerospace industry is devoted to improving the aircraft performance while reducing its weight and limiting the emissions. Part of this objective can be accomplished with the use of high-performance long fibre reinforced polymer laminated composites. Being the first mode of damage under loading, intralaminar cracks initiate at the free edge of the off-axis plies and propagate along the respective fibre orientation. While these cracks grow as tunnels and increase in number, at some point two close cracks in plies of different off-axis orientation could intersect forming an envelope with the free edge. As loading continues, local delamination is expected within this envelope. The evolution and interactions of the different damage modes and the accumulation of damage under a specific loading are crucial in order to have a good understanding of the mechanisms and hence an accurate prediction of the mechanical properties´ degradation. This thesis is devoted to initiation and evolution of intralaminar cracking in plies and interlayer delamination in composite laminates. In the first part, quasi-isotropic Carbon Fibre/ Epoxy non-crimp fabric (NCF) laminates were studied under both quasi-static and cyclic loadings. The objective was to develop an efficient testing methodology for statistical damage evolution determination in Fatigue. The sequence of damage occurrences (intralaminar cracks in the different layers, delaminations at the different interfaces) loaded under quasi-static and tension-tension fatigue is first captured. To save characterisation time and costs, a simple model for predicting intralaminar cracking in laminates under cyclic loads was proposed and validated under low stress cyclic loads and low crack density. The model is based on Weibull distribution for the probability of cracking where part of parameters is obtained in quasi-static tests and part in a limited number of cyclic tests. The predictions of dependency of the cracking on the stress and number of cycles are validated against experimental observations of cracking in the 90-plies of quasi-isotropic NCF laminates as well as in tape based cross-ply laminates. In position where intralaminar cracks meet the specimen edge, local delaminations initiate due to the high 3D stress state. The delamination is further assisted by cracks in other off-axis plies, usually linking them. The average delamination length dependence on loading parameters is characterized and linked with the extent of the laminate stiffness reduction, showing using a simple ply-discount analysis that delaminations are the main reason for very large axial modulus reduction. In the second part, local delaminations and their effect on laminate stiffness are analysed using FEM. Expressions for the crack opening displacement (COD) determined using FEM are obtained and a modelling approach based on GLOB-LOC is performed for intralaminar crack case with local delaminations starting from the intralaminar crack. The delamination length is used as a parameter and studies are performed for different materials. Strong effect of delaminations on COD and on the axial modulus of the laminate is found. Finally, the last findings are used to simulate the damaged composite laminate behaviour in 4-point bending test. The bending stiffness of the laminate is significantly reduced by intralaminar cracks with delaminations. An approach, using the concept of the effective stiffness of the damaged ply is used. The so obtained effective stiffness matrix is a function of intralaminar crack density in the ply and the delamination length. The effective stiffness is used to calculate the bending stiffness of the damaged laminate. The laminate curvature calculated in this way is in a very good agreement with the curvature obtained in 3-D FEM simulations of the test with explicitly including cracks and delaminations in the model
Actes de conférences sur le sujet "Laminate composite NCF"
Soltani, Seyed A., Gena Le et Ramazan Asmatulu. « Mechanical Properties of Out-of-Autoclave Non-Crimp Fabric Epoxy Composites for Manufacturing Plant Elevations ». Dans ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/imece2014-39771.
Texte intégralZENG, YU, et JOHN MONTESANO. « MULTISCALE FE MODELLING AND ANN TO PREDICT MECHANICAL PROPERTIES OF NON-CRIMP FABRIC COMPOSITES WITH MANUFACTURING INDUCED DEFECTS ». Dans Proceedings for the American Society for Composites-Thirty Eighth Technical Conference. Destech Publications, Inc., 2023. http://dx.doi.org/10.12783/asc38/36608.
Texte intégralSURATKAR, AADITYA, JOHN MONTESANO et JEFFREY WOOD. « DAMAGE EVOLUTION IN NON-CRIMP FABRIC CARBON FIBER/EPOXY MULTI-DIRECTIONAL LAMINATES UNDER QUASI-STATIC TENSION ». Dans Thirty-sixth Technical Conference. Destech Publications, Inc., 2021. http://dx.doi.org/10.12783/asc36/35921.
Texte intégralPatlolla, V., J. George, Soo-Han Loo et R. Asmatulu. « Effects of UV Light and Moisture Absorption on the Impact Resistance of Three Different Carbon Fiber-Reinforced Composites ». Dans ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/imece2014-39999.
Texte intégralLIU, XIN, SÉRGIO COSTA, BANGDE LIU et SARTHAK TREHAN. « CONVOLUTIONAL NEURAL NETWORK FOR PREDICTING MECHANICAL BEHAVIOR OF COMPOSITES WITH FIBER WAVINESS ». Dans Proceedings for the American Society for Composites-Thirty Seventh Technical Conference. Destech Publications, Inc., 2022. http://dx.doi.org/10.12783/asc37/36382.
Texte intégralBadagi, Vijay Kumar, et Rajamohan Ganesan. « Vibration and Buckling Response of Width Tapered Laminated Composite Beams Using Ritz Method for Rotorcraft Blade ». Dans ASME 2010 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/detc2010-28214.
Texte intégralJadhav, Vishwas S., et Ajit D. Kelkar. « Fabrication, Processing and Characterization of Carbon Fibre Reinforced Laminated Composite Embedded With Graphene Lattice Sheets ». Dans ASME 2021 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/imece2021-71191.
Texte intégralKaliappan, S., et L. Natrayan. « Revolutionizing Automotive Materials through Enhanced Mechanical Properties of Epoxy Hybrid Bio-Composites with Hemp, Kenaf, and Coconut Powder ». Dans International Conference on Trends in Automotive Parts Systems and Applications. 400 Commonwealth Drive, Warrendale, PA, United States : SAE International, 2024. http://dx.doi.org/10.4271/2023-01-5185.
Texte intégralPalmieri, Frank, Tyler Hudson, Roberto Cano, Erik Tastepe, Dean Rufeisen, Luay Ahmed, Yi Lin, Christopher Wohl et John Connell. « Reliable Bonding of Composite Laminates Using Reflowable Epoxy Resins ». Dans SAMPE 2019 - Charlotte, NC. SAMPE, 2019. http://dx.doi.org/10.33599/nasampe/s.19.1416.
Texte intégralVakili Rad, Cyrus, Frank Thomas, Subramani Sockalingam et Zafer Gurdal. « Low Velocity Impact Response of Hybrid Pseudo-Woven Fiber-Reinforced Composite Laminates ». Dans SAMPE 2019 - Charlotte, NC. SAMPE, 2019. http://dx.doi.org/10.33599/nasampe/s.19.1473.
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