黄春芳等：薄铺层复合材料薄壁管轴压屈曲行为研究 ·863· [2]Fuller J D,Wisnom M R.Pseudo-ductility and damage suppres- ched thin ply laminates using finite fracture mechanics and the sion in thin ply CFRP angle-ply laminates.Composites Part A, phase field approach.Compos Sci Technol,2017,150:205 2015.69:64 [12]Sebaey T A,Mahdi E.Using thin-plies to improve the damage [3]Borg C.An introduction to spread tow reinforcements:Part 1-man- resistance and tolerance of aeronautical CFRP composites.Com- ufacture and properties.Reinf Plast,2015,59(4):194 posites Part A,2016,86:31 [4]EL-Dessouky H M,Lawrence C A.Ultra-lightweight carbon fibre/ [13]Cheng S.Ho B PC.Stability of heterogeneous anisotropic eylin- themmoplastic composite material using spread tow technology. drical shells under combined loading.AlAA J,1963,1(4):892 Composites Part B.2013,50:91 [14]Jones R M.Buckling of circular cylindrical shells with multiple [5]He M C,Huang C F,Zheng Q,et al.Progress of research on orthotropic layers and eccentric stiffeners.AlAA J,1968,6 thin-ply laminated composites.Fiber Reinf Plast/Compos,2016 (12):2301 (8):92 [15]Bisagni C.Cordisco P.An experimental investigation into the (何明昌，黄春芳，郑青，等.薄铺层层合复合材料研究进展 buckling and post-buckling of CFRP shells under combined axial 玻璃钢复合材料，2016(8)：92) and torsion loading.Compos Struct,2003,60(4):391 [6]Yuan Y N,Wang S.Yang H,et al.Analysis of pseudo-ductility [16]Chen R X.Axial compression stability of the composite case.J in thin-ply carbon fiber angle-ply laminates.Compos Struct,2017, Solid Rocket Technol,2001,24(1):13 180:876 (陈汝训.复合材料壳体的轴压稳定性.固体火箭技术， [7]Yamashita S,Sonehara T,Takahashi J,et al.Effect of thin-ply 2001,24(1):13) on damage behaviour of continuous and discontinuous carbon fibre [17]Zhu R J.Li F,Zhang H M.A model for critical buckling load of reinforced thermoplastics subjected to simulated lightning strike. thin composite tube based on elastic foundation beam theory.Acta Composites Part A,2017,95:132 Mater Compos Sin,2017,34(8):1745 [8]Yuan Y N,Yao X F,Liu B,et al.Failure modes and strength (朱锐杰，李峰，张恒铭.基于弹性基础梁理论的复合材料 prediction of thin ply CFRP angle-ply laminates.Compos Struct. 薄壁圆柱壳屈曲承载力模型.复合材料学报，2017,34(8)： 2017,176:729 1745) [9]Saito H,Takeuchi H.Kimpara I.A study of crack suppression [18]Weaver P M,Driesen J R,Roberts P.Anisotropic effects in the mechanism of thin-ply carbon-fiber-reinforced polymer laminate compression buckling of laminated composite cylindrical shells. with mesoscopic numerical simulation.Compos Mater,2014,48 Compos Sci Technol,2002,62(1):91 (17):2085 [19]Soutis C.Compressive strength of composite laminates with an [10]Amacher R,Cugnoni J,Botsis J,et al.Thin ply composites:ex- open hole:effect of ply blocking.J Compos Mater,2013,47 perimental characterization and modeling of size-effects.Compos (20-21):2503 Sci Technol,2014,101:121 [20]Chamis CC.Buckling of anisotropic composites plates.Struct [11]Reinoso J,Arteiro A,Paggi M,et al.Strength prediction of not- Diis,1969,95(10):2119黄春芳等: 薄铺层复合材料薄壁管轴压屈曲行为研究 [2] Fuller J D, Wisnom M R. Pseudo鄄ductility and damage suppres鄄 sion in thin ply CFRP angle鄄ply laminates. Composites Part A, 2015, 69: 64 [3] Borg C. An introduction to spread tow reinforcements: Part 1鄄man鄄 ufacture and properties. Reinf Plast, 2015, 59(4): 194 [4] EL鄄Dessouky H M, Lawrence C A. Ultra鄄lightweight carbon fibre / thermoplastic composite material using spread tow technology. Composites Part B, 2013, 50: 91 [5] He M C, Huang C F, Zheng Q, et al. Progress of research on thin鄄ply laminated composites. Fiber Reinf Plast / Compos, 2016 (8): 92 (何明昌, 黄春芳, 郑青, 等. 薄铺层层合复合材料研究进展. 玻璃钢复合材料, 2016(8): 92) [6] Yuan Y N, Wang S, Yang H, et al. Analysis of pseudo鄄ductility in thin鄄ply carbon fiber angle鄄ply laminates. Compos Struct, 2017, 180: 876 [7] Yamashita S, Sonehara T, Takahashi J, et al. Effect of thin鄄ply on damage behaviour of continuous and discontinuous carbon fibre reinforced thermoplastics subjected to simulated lightning strike. Composites Part A, 2017, 95: 132 [8] Yuan Y N, Yao X F, Liu B, et al. Failure modes and strength prediction of thin ply CFRP angle鄄ply laminates. Compos Struct, 2017, 176: 729 [9] Saito H, Takeuchi H, Kimpara I. A study of crack suppression mechanism of thin鄄ply carbon鄄fiber鄄reinforced polymer laminate with mesoscopic numerical simulation. J Compos Mater, 2014, 48 (17): 2085 [10] Amacher R, Cugnoni J, Botsis J, et al. Thin ply composites: ex鄄 perimental characterization and modeling of size鄄effects. Compos Sci Technol, 2014, 101: 121 [11] Reinoso J, Arteiro A, Paggi M, et al. Strength prediction of not鄄 ched thin ply laminates using finite fracture mechanics and the phase field approach. Compos Sci Technol, 2017, 150: 205 [12] Sebaey T A, Mahdi E. Using thin鄄plies to improve the damage resistance and tolerance of aeronautical CFRP composites. Com鄄 posites Part A, 2016, 86: 31 [13] Cheng S, Ho B P C. Stability of heterogeneous anisotropic cylin鄄 drical shells under combined loading. AIAA J, 1963, 1(4): 892 [14] Jones R M. Buckling of circular cylindrical shells with multiple orthotropic layers and eccentric stiffeners. AIAA J, 1968, 6 (12): 2301 [15] Bisagni C, Cordisco P. An experimental investigation into the buckling and post鄄buckling of CFRP shells under combined axial and torsion loading. Compos Struct, 2003, 60(4): 391 [16] Chen R X. Axial compression stability of the composite case. J Solid Rocket Technol, 2001, 24(1): 13 (陈汝训. 复合材料壳体的轴压稳定性. 固体火箭技术, 2001, 24(1): 13) [17] Zhu R J, Li F, Zhang H M. A model for critical buckling load of thin composite tube based on elastic foundation beam theory. Acta Mater Compos Sin, 2017, 34(8): 1745 (朱锐杰, 李峰, 张恒铭. 基于弹性基础梁理论的复合材料 薄壁圆柱壳屈曲承载力模型. 复合材料学报, 2017, 34(8): 1745) [18] Weaver P M, Driesen J R, Roberts P. Anisotropic effects in the compression buckling of laminated composite cylindrical shells. Compos Sci Technol, 2002, 62(1): 91 [19] Soutis C. Compressive strength of composite laminates with an open hole: effect of ply blocking. J Compos Mater, 2013, 47 (20鄄21): 2503 [20] Chamis C C. Buckling of anisotropic composites plates. J Struct Divis, 1969, 95(10): 2119 ·863·