Littérature scientifique sur le sujet « Interlaminar and intralaminar damage »
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Articles de revues sur le sujet "Interlaminar and intralaminar damage"
Keršienė, Neringa, et Antanas Žiliukas. « INTERLAMINAR AND INTRALAMINAR DAMAGE MECHANISMS OF IMPACT RESISTANT AIRCRAFT MATERIALS UNDER LOW‐ENERGY IMPACT ». Aviation 10, no 3 (30 septembre 2006) : 3–8. http://dx.doi.org/10.3846/16487788.2006.9635933.
Texte intégralBruno, Domenico, Fabrizio Greco et Paolo Lonetti. « Interaction Between Interlaminar and Intralaminar Damage in Fiber-Reinforced Composite Laminates ». International Journal for Computational Methods in Engineering Science and Mechanics 9, no 6 (30 septembre 2008) : 358–73. http://dx.doi.org/10.1080/15502280802365824.
Texte intégralLi, N., P. H. Chen et Q. Ye. « A damage mechanics model for low-velocity impact damage analysis of composite laminates ». Aeronautical Journal 121, no 1238 (6 mars 2017) : 515–32. http://dx.doi.org/10.1017/aer.2017.6.
Texte intégralLiao, BB, et PF Liu. « Finite element analysis of dynamic progressive failure properties of GLARE hybrid laminates under low-velocity impact ». Journal of Composite Materials 52, no 10 (10 août 2017) : 1317–30. http://dx.doi.org/10.1177/0021998317724216.
Texte intégralDuplessis Kergomard, Y., J. Renard, A. Thionnet et C. Landry. « Intralaminar and interlaminar damage in quasi-unidirectional stratified composite structures : Experimental analysis ». Composites Science and Technology 70, no 10 (30 septembre 2010) : 1504–12. http://dx.doi.org/10.1016/j.compscitech.2010.05.006.
Texte intégralHassoon, Omar H., Mayyadah S. Abed, Jawad K. Oleiwi et M. Tarfaoui. « Experimental and numerical investigation of drop weight impact of aramid and UHMWPE reinforced epoxy ». Journal of the Mechanical Behavior of Materials 31, no 1 (1 janvier 2022) : 71–82. http://dx.doi.org/10.1515/jmbm-2022-0008.
Texte intégralZou, Z., S. R. Reid, S. Li et P. D. Soden. « Modelling Interlaminar and Intralaminar Damage in Filament-Wound Pipes under Quasi-Static Indentation ». Journal of Composite Materials 36, no 4 (février 2002) : 477–99. http://dx.doi.org/10.1177/0021998302036004539.
Texte intégralBALZANI, CLAUDIO, et WERNER WAGNER. « NUMERICAL TREATMENT OF DAMAGE PROPAGATION IN AXIALLY COMPRESSED COMPOSITE AIRFRAME PANELS ». International Journal of Structural Stability and Dynamics 10, no 04 (octobre 2010) : 683–703. http://dx.doi.org/10.1142/s0219455410003683.
Texte intégralMeon, M. S., N. H. Mohamad Nor, S. Shawal, J. B. Saedon, M. N. Rao et K. U. Schröder. « On the Modelling Aspect of Low-Velocity Impact Composite Laminates ». journal of Mechanical Engineering 17, no 2 (15 juillet 2020) : 13–25. http://dx.doi.org/10.24191/jmeche.v17i2.15297.
Texte intégralTownsend, Patrick, Juan Carlos Suárez, Paz Pinilla et Nadia Muñoz. « Insertion of a Viscoelastic Layer to Reduce the Propagation of Energy by Vertical Impacts of Slamming in Planing Hull Vessels ». Key Engineering Materials 889 (16 juin 2021) : 65–70. http://dx.doi.org/10.4028/www.scientific.net/kem.889.65.
Texte intégralThèses sur le sujet "Interlaminar and intralaminar damage"
González, Juan Emilio Vicente. « Simulation of interlaminar and intralaminar damage in polymer-based composites for aeronautical applications under impact loading ». Doctoral thesis, Universitat de Girona, 2011. http://hdl.handle.net/10803/22834.
Texte intégralThe application of polymer-based composites reinforced by long fibers, called advanced Fiber Reinforced Plastic (FRP), is gradually increasing as a result of their good specific mechanical properties and increased flexibility of design. One of the largest consumers is the aerospace industry, since the application of these materials has clear economic and environmental benefits. When composites are to be used in structural components, a design development program is initiated, where a combination of testing and analysis techniques is typically performed. The development of reliable analysis tools that enable to understand the structure mechanical behavior, as well as to replace most, but not all, the real experimental tests, is of clear interest. Susceptibility to damage from concentrated out-of-plane impact forces is one of the major design concerns of structures made of advanced FRPs used in the aerospace industry. Lack of knowledge of the impact effects on these structures is a factor in limiting the use of composite materials. Therefore, the development of virtual mechanical testing models to analyze the impact damage resistance of a structure is of great interest, but even more, the prediction of the post-impact residual strength. In this sense, the present thesis covers a wide range of analysis of the low-velocity and large mass impact events on monolithic, flat, rectangular, polymer-based laminated composite plates with conventional stacking sequences. Keeping in mind that the main goal of this work is the prediction of the residual compressive strength of an impacted specimen coupon, a set of different tasks are performed in order to provide suitable tools to analyze the problem. Accordingly, the topics which are addressed in this thesis are: the analytical description of the impact, the design and the realization of an experimental test plan, the formulation and implementation of constitutive models for the description of the composite material behavior, and the assessment of the performance of virtual tests based on finite element models where the constitutive models are used.
Sebaey, Abdella Tamer Ali Abdella. « Characterization and optimization of dispersed composite laminates for damage resistant aeronautical structures ». Doctoral thesis, Universitat de Girona, 2013. http://hdl.handle.net/10803/98393.
Texte intégralEl principal objectiu de la tesi és valorar la resistència al dany i la tolerància al dany dels laminats no-convencionals dispersos i comparar la seva resposta amb la dels laminats convencionals. No obstant, part de l'atenció es dedica a comprendre el comportament de la delaminació en laminats multidireccionals. En la primera part de la tesi, s'analitza la delaminació en laminats multidireccionals. L'objectiu és dissenyar una seqüència d'apilament apropiada per evitar el dany intralaminar (migració de la delaminació) i permetre la caracterització de la tenacitat a la fractura en model. Els resultats d'aquests estudi mostren que a major rigidesa a flexió dels braços de l'esquerda, menor és la tendència a la migració de l'esquerda. Aquest aspecte també s'ha analitzat experimentalment, obtenint les mateixes conclusions.
Akterskaia, Margarita [Verfasser]. « Global-local progressive failure analysis of composite panels including skin-stringer debonding and intralaminar damage / Margarita Akterskaia ». Hannover : Gottfried Wilhelm Leibniz Universität Hannover, 2019. http://d-nb.info/1193177200/34.
Texte intégralMaziz, Ammar. « Analyse des endommagements dans les pipes en matériaux composites ». Electronic Thesis or Diss., Brest, École nationale supérieure de techniques avancées Bretagne, 2021. http://www.theses.fr/2021ENTA0019.
Texte intégralDamage modelling of hybrid composite materials has played an important role in the design of composite structures. Although numerical models for the progressive damage of filament wound hybrid composite pipes such, matrix cracking, delamination, and fiber failure have been developed in the literature; there is still a need for improvement. This thesis aims to develop damage models suitable for predicting dynamic behaviour and intra-laminar and inter-laminar damage in hybrid composite tubes under internal pressure subjected to dynamic loading such as the impact of an external object. Fracture mechanics and continuum damage mechanics approaches were adopted to build the damage model. A detailed analysis was performed to have an overview of all the damage mechanisms until the final failure. Cohesive elements were inserted into the two-dimensional and three-dimensional models to simulate the initiation and propagation of matrix cracking and delamination in cross-layered laminates. The damage model was implemented in the FE code (Abaqus/Explicit) by a user-defined material subroutine (VUMAT). Subsequently, validations based on test/calculation correlations on real subsystems and/or parts were performed. Damage initiation was predicted based on the stress-strain failure criteria, while the damage evolution law was based on the dissipation of failure energy. The nonlinear behavior of the material in shear was also taken into account and validated against experimental/numerical results. The predictions show excellent agreement with the experimental observations
Farge, Laurent. « Caractérisation de l'endommagement de matériaux composites stratifiés à l'aide de la mesure du déplacement par une méthode optique plein-champ ». Thesis, Vandoeuvre-les-Nancy, INPL, 2009. http://www.theses.fr/2009INPL052N/document.
Texte intégralThis work results from a collaboration between Pr Ayadi (Institut Polytechnique de Lorraine) and Pr Varna (Technical University of Luleå). Since 2005, Pr Varna has developed an original method that allows for the determination of all the thermoelastic constants of a damaged laminate. The stiffness reduction is governed by two parameters: the average value of the opening and the average value of the sliding of the crack surfaces. These values are normalized with respect to the applied loading. In this work, the potential of speckle interferometry is analysed to obtain these two parameters. More generally, we show the usefulness of displacement field measurements to characterize damage development in laminates. The first chapter is dedicated to the damage that occurs in laminates. The main objective is to highlight the points for which displacement field measurements could bring interesting information. In the second chapter, the principle of speckle interferometry is described. The choice of this technique for the considered application is discussed and justified. In the third chapter, an experimental study of the potential of speckle interferometry is proposed to characterize the damage forms that occur in a glass/epoxy laminate. In the last chapter, the development of damage is experimentally analysed in a carbon/epoxy laminate
Orifici, Adrian Cirino, et adrian orifici@student rmit edu au. « Degradation Models for the Collapse Analysis of Composite Aerospace Structures ». RMIT University. Aerospace, Mechanical and Manufacturing Engineering, 2007. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20080619.090039.
Texte intégralIervolino, Onorio. « Enhanced impact resistance and pseudo plastic behaviour in composite structures through 3D twisted helical arrangement of fibres and design of a novel chipless sensor for damage detection ». Thesis, University of Bath, 2017. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.723326.
Texte intégralBen, Kahla Hiba. « Models for bending stiffness in laminates with intralaminar and interlaminar damage ». Thesis, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-44595.
Texte intégralLivres sur le sujet "Interlaminar and intralaminar damage"
German, Janusz. Intralaminar damage in fiber-reinforced polymeric matrix laminates. Cracow : Cracow University of Technology, 2004.
Trouver le texte intégralIllg, Walter. Effect of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminates. Hampton, Va : Langley Research Center, 1986.
Trouver le texte intégralGrami, Vahid, Salim M. Hayek et Samer N. Narouze. Lumbar Transforaminal and Nerve Root Injections : Fluoroscopy. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780199908004.003.0016.
Texte intégralChapitres de livres sur le sujet "Interlaminar and intralaminar damage"
Huchette, Cédric, Thomas Vandellos et Frédéric Laurin. « Influence of Intralaminar Damage on the Delamination Crack Evolution ». Dans Springer Aerospace Technology, 107–40. Cham : Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-04004-2_5.
Texte intégralMassabò, Roberta. « Effective Modeling of Interlaminar Damage in Multilayered Composite Structures Using Zigzag Kinematic Approximations ». Dans Handbook of Damage Mechanics, 1–34. New York, NY : Springer New York, 2020. http://dx.doi.org/10.1007/978-1-4614-8968-9_91-1.
Texte intégralMassabò, Roberta. « Effective Modeling of Interlaminar Damage in Multilayered Composite Structures Using Zigzag Kinematic Approximations ». Dans Handbook of Damage Mechanics, 665–98. Cham : Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-60242-0_91.
Texte intégralPrinz, R. « Damage Rates for Interlaminar Failure of Fatigued CFRP Laminates ». Dans Developments in the Science and Technology of Composite Materials, 189–94. Dordrecht : Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-0787-4_23.
Texte intégralLi, Lei, et Zhu Feng Yue. « Analysis of Interlaminar Stresses and Failure around Hole Edge for Composite Laminates under In-Plane Loading ». Dans Fracture and Damage Mechanics V, 1027–30. Stafa : Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-413-8.1027.
Texte intégralShimamura, Y., A. Todoroki et H. Kobayashi. « Intralaminar and Interlaminar Fracture Growth Simulation of Composite Plates Based on Finite Element Method by Using Plane Elements ». Dans Design and Manufacturing of Composites, 149–53. New York : CRC Press, 2021. http://dx.doi.org/10.1201/9781003076131-28.
Texte intégralBilal Afzal, Muhammad. « Modeling of Damage Evolution of Fiber-Reinforced Composite Structure ». Dans Safety and Risk Assessment of Civil Aircraft during Operation. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.93323.
Texte intégralIsa, Tadashi, Masatoshi Kasai et Richard Veale. « The Superior Colliculus ». Dans Handbook of Brain Microcircuits, sous la direction de Gordon M. Shepherd et Sten Grillner, 457–66. Oxford University Press, 2017. http://dx.doi.org/10.1093/med/9780190636111.003.0039.
Texte intégralVarandas, L. F., G. Catalanotti, A. Arteiro, António R. Melro et B. G. Falzon. « Micromechanical modelling of interlaminar damage propagation and migration ». Dans Multi-Scale Continuum Mechanics Modelling of Fibre-Reinforced Polymer Composites, 307–47. Elsevier, 2021. http://dx.doi.org/10.1016/b978-0-12-818984-9.00011-1.
Texte intégralForghani, A., M. Shahbazi, N. Zobeiry, A. Poursartip et R. Vaziri. « An overview of continuum damage models used to simulate intralaminar failure mechanisms in advanced composite materials ». Dans Numerical Modelling of Failure in Advanced Composite Materials, 151–73. Elsevier, 2015. http://dx.doi.org/10.1016/b978-0-08-100332-9.00006-2.
Texte intégralActes de conférences sur le sujet "Interlaminar and intralaminar damage"
Özkaya, Özge, et Altan Kayran. « Nonlinear Static Aeroelastic Behavior of Composite Missile Fin with Interlaminar and Intralaminar Damage ». Dans 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1449.
Texte intégralMEYER, CHRISTOPHER S., BAZLE Z. HAQUE, DANIEL J. O’BRIEN et OHN W. GILLESPIE, JR. « MICROMECHANICAL FINITE ELEMENT PREDICTION OF INTERLAMINAR TRACTION-SEPARATION LAWS USING J-INTEGRAL APPROACH ». Dans Thirty-sixth Technical Conference. Destech Publications, Inc., 2021. http://dx.doi.org/10.12783/asc36/35941.
Texte intégralNIETO, ZACKERY, EDGAR AVALOS, VIPUL RANATUNGA et ALEJANDRA CASTELLANOS. « ASSESSMENT ON THE CAPABILITIES OF ABAQUS AND LS-DYNA TO PREDICT THE BEHAVIOR OF LAMINATED COMPOSITES SUBJECTED TO LOW-VELOCITY IMPACTS ». Dans Proceedings for the American Society for Composites-Thirty Seventh Technical Conference. Destech Publications, Inc., 2022. http://dx.doi.org/10.12783/asc37/36430.
Texte intégralTiano, Thomas, Margaret Roylance, Benjamin Harrison et Richard Czerw. « Intralaminar Reinforcement for Biomimetic Toughening of Bismaleimide Composites Using Nanostructured Materials ». Dans ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-81689.
Texte intégralGoyal-Singhal, Vinay, Navin Jaunky, Eric Johnson et Damodar Ambur. « Intralaminar and Interlaminar Progressive Failure Analyses of Composite Panels with Circular Cutouts ». Dans 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/10.2514/6.2002-1745.
Texte intégralVENKATESAN, KARTHIK RAJAN, et ADITI CHATTOPADHYAY. « Multiscale Analysis for Interlaminar and Intralaminar Reinforcement of Composite Laminates with Carbon Nanotube Architecture ». Dans American Society for Composites 2019. Lancaster, PA : DEStech Publications, Inc., 2019. http://dx.doi.org/10.12783/asc34/31387.
Texte intégralMohite, Preetamkumar, Gilles Lubineau, Pierre Ladeveze et Ana-cristina Galucio. « Validation of Intralaminar Behaviour of the Laminated Composites by Damage Mesomodel ». Dans 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2422.
Texte intégralBedsole, Robert, et Hareesh Tippur. « Interlaminar and Intralaminar Dynamic Fracture Behaviors of CFRP : An Investigation Using Digital Image Correlation and High-Speed Photography ». Dans 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0892.
Texte intégralNgabonziza, Yves, Claudia Boldrini, Benjamin Liaw, Jackie Li et Feridun Delale. « Damage Self-Diagnosis in Carbon Fiber-Reinforced Composites Under Fatigue Loading ». Dans ASME 2010 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. ASMEDC, 2010. http://dx.doi.org/10.1115/smasis2010-3870.
Texte intégralHYDER, IMRAN, JOSEPH SCHAEFER, BRIAN JUSTUSSON, STEVE WANTHAL, FRANK LEONE et CHERYL ROSE. « Assessment of Intralaminar Progressive Damage and Failure Analysis Methods Using an Efficient Evaluation Framework ». Dans American Society for Composites 2017. Lancaster, PA : DEStech Publications, Inc., 2017. http://dx.doi.org/10.12783/asc2017/15405.
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