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CONTACT ANALYSIS FOR FIBER-REINFORCED, DELAMINATED LAMINATES WITH KINEMATIC NONLINEARITY 被引量:7

CONTACT ANALYSIS FOR FIBER-REINFORCED, DELAMINATED LAMINATES WITH KINEMATIC NONLINEARITY
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摘要 A macro-micro analytical approach for the anti-penetrating contact problem at the interfaces of the delamination in symmetrically cross-plied,fiber-reinforced rectangular laminates is presented in this paper.The laminate is simply supported and subjected to a uniform transverse load with a through-width delamination buried at the center position.A contact factor is defined to characterize the contact effect and determined using the micro-mechanics of composite material.By analyzing the kinematics of nonlinear deformation at the interfaces of the delamination,the contact force is derived.Asymptotic solutions from perturbation analysis are presented.It is found that the deformation of the laminate involves a global deflection and a local buckling.The antipenetrating contact effects are characterized by the local buckling and are intrinsic properties of the laminates,relying only on the geometries of the delamination and the material properties.Parametric analyses show that the location and size of the contact areas and the distribution of the contact force are hardly affected by the aspect ratio. A macro-micro analytical approach for the anti-penetrating contact problem at the interfaces of the delamination in symmetrically cross-plied,fiber-reinforced rectangular laminates is presented in this paper.The laminate is simply supported and subjected to a uniform transverse load with a through-width delamination buried at the center position.A contact factor is defined to characterize the contact effect and determined using the micro-mechanics of composite material.By analyzing the kinematics of nonlinear deformation at the interfaces of the delamination,the contact force is derived.Asymptotic solutions from perturbation analysis are presented.It is found that the deformation of the laminate involves a global deflection and a local buckling.The antipenetrating contact effects are characterized by the local buckling and are intrinsic properties of the laminates,relying only on the geometries of the delamination and the material properties.Parametric analyses show that the location and size of the contact areas and the distribution of the contact force are hardly affected by the aspect ratio.
出处 《Acta Mechanica Solida Sinica》 SCIE EI CSCD 2013年第4期388-402,共15页 固体力学学报(英文版)
基金 supported by the National Natural Science Foundation of China(Nos.11172113 and 11032005)
关键词 rectangular laminate DELAMINATION contact effect perturbation approach nonlinear analysis rectangular laminate delamination contact effect perturbation approach nonlinear analysis
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  • 1Whitcomb,J.D. Analysis of a laminate with a postbuckled embedded delamination, including contact ef- fects. Journal of Composite Materials, 1992, 26(10): 1523-1535.
  • 2Yeh,M.K. Fang,L.B. and Kao,M.H. Bending behavior of delaminated composite plates with contact eicects. Composite Structures, 1997, 39(3-4): 347-356.
  • 3Yeh,M.K. and Fang,L.B. Contact analysis and experiment of delaminated cantilever composite beam. Composites: Part B, 1999, 30: 407-414.
  • 4Chen,H. and Bai,R. Postbuckling behavior of face/core debonded composite sandwich plate considering matrix crack and contact effect. Compos. Struct. 2002, 57: 305-313.
  • 5Frostig,Y. and Thomsen,O.T. Non-linear behavior of delaminated unidirectional sandwich panels with partial contact and a transversely flexible core. International Journal of Non-Linear Mechanics, 2005, 40: 633-651.
  • 6Zhu,F. Fu,Y. and Chen,D. Analysis of fatigue delamination growth for piezoelectric laminated cylindrical shell considering nonlinear contact effect. International Journal of Solids and Structures, 2008, 45: 5381- 5396.
  • 7Hu,N. Fukunaga,H. Sekine,H. and Mohammad Ali K. Compressive buckling of laminates with an em- bedded delamination. Composites Science and Technology, 1999, 59: 1247-1260.
  • 8Bruno,D. Greco,F. and Lonetti,P. A coupled interface-multilayer approach for mixed mode delamination and contact analysis in laminated composites. International Journal of Solids and Structures, 2003, 40: 7245-7268.
  • 9Chen,H.R. Wang,M. and Bai,R.X. The effect of nonlinear contact upon natural frequency of delaminated stiffened composite plate. Composite Strictures, 2006, 76: 28-33.
  • 10Chen,H.R. Hong,M. and Liu,Y.D. Dynamic behavior of delaminated plates considering progressive tallure process. Composite Structures, 2004, 66: 456-466.

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