Test of multiimpact damage and highcycle shear fatigue of stiffened composite panels
-
摘要: 为研究多点冲击损伤和高周剪切疲劳对复合材料加筋壁板损伤演化、屈曲行为及破坏模式的影响,制作了9块相同构型的复合材料加筋壁板,设计了冲击试验、高周剪切疲劳试验和剩余剪切强度试验。在多点冲击和高周剪切疲劳试验过程中,使用超声C扫描系统监测了损伤区域。C扫描图像表明损伤区域的长度和宽度随着循环次数的增加而增加。与无预制损伤试验件相比,多点冲击损伤和高周剪切疲劳试验件的平均破坏载荷下降了约50%。冲击或疲劳形成的初始损伤对破坏模式产生影响,冲击疲劳试验件出现了局部蒙皮屈曲变形,破坏裂纹非常接近冲击点。Abstract: To study the effect of multiimpact damage and highcycle shear fatigue on the damage evolution, buckling behavior and failure modes of stiffened composite panels, nine stiffened composite panels were manufactured with similar configurations, and the impact test, highcycle shear fatigue test and residual shear strength test were designed. During the multiimpact and highcycle shear fatigue tests, the damaged zones were detected by the ultrasonic Cscan system. Cscan images indicated that the length and width of damaged zones increased with the increasing number of cycles. Compared with initial undamaged specimen, the average failure load of specimens with multiimpact damage and highcycle shear fatigue declined about 50%. Furthermore, the failure modes of the specimens were also affected by the initial damage caused by impact or fatigue. For the impact and fatigue specimens, the deformation of local buckling skin appeared, and the failure cracks were much near the impact damaged zones.
-
[1] 中国航空研究院.复合材料结构设计手册[M].北京:航空工业出版社,2001:477-478. [2] ABRATE S.Impact on laminated composite materials[J].Applied Mechanics Reviews,1991,44(4):155-190. [3] ABRATE S.Impact on laminated materials:recent advances[J].Applied Mechanics Reviews,1994,47(11):517-544. [4] SANCHEZSAEZ S,BARBERO E,ZAERA R,et al.Compression after impact of thin composite laminates[J].Composite Science and Technology,2005,65(13):1911-1919. [5] RHEAD A T,MARCHANT D,BUTLE R.Compressive strength of composite laminates following free edge impact[J].Composites:Part A Applied Science and Manufacturing,2009,41(9):1056-1065. [6] RICHARDSON M O W,WISHEART M J.Review of lowvelocity impact properties of composite materials[J].Composites:Part A Applied Science and Manufacturing,1996,27(12):1123-1131. [7] MITREVSKI T,MARSHALL I H,THOMSON R.The influence of impactor shape on the damage to composite laminates[J].Composite Structures,2006,76(1/2):116-122. [8] 张铁军,李曙林,常飞,等.多损伤复合材料加筋壁板高周疲劳特性及剩余压缩强度[J].复合材料学报,2015,32(6):1754-1761.ZHANG Tiejun,LI Shulin,CHANG Fei,et al.High cycle fatigue characteristics and residual compressive strength of stiffened composite panels with multidamage[J].Acta Materiae Compositae Sinica,2015,32(6):1754-1761.(in Chinese) [9] 崔海坡,温卫东,徐颖.复合材料板冲击损伤及剩余拉伸强度试验[J].航空动力学报,2007,22(10):1742-1747.CUI Haipo,WEN Weidong,XU Ying.Experimental research on impact damage and residual tensile strength of composite laminates[J].Journal of Aerospace Power,2007,22(10):1742-1747.(in Chinese) [10] 石晓朋,李曙林,常飞,等.复合材料加筋壁板低速冲击响应与能量关系研究[J].材料工程,2015,43(4):53-58.SHI Xiaopeng,LI Shulin,CHANG Fei,et al.Connection of lowvelocity impact response and impact energy of stiffened composite panel[J].Journal of Materials Engineering,2015,43(4):53-58.(in Chinese) [11] RIVALLANT S,BOUVET C,ABDALLAH E A,et al.Experimental analysis of CFRP laminates subjected to compression after impact:the role of impactinduced cracks in failure[J].Composite Structures,2014,111(1):147-157. [12] MARGUERES P,MERAGHNI F,BENZEGGAGH M L.Comparison of stiffness measurements and damage investigation techniques for a fatigued and postimpact fatigued GFRP composite obtained by RTM process[J].Composites:Part A Applied Science and Manufacturing,2000,31(2):151-163. [13] CHEN A S,ALMOND D P,HARRIS B.Impact damage growth in composites under fatigue conditions monitored by acoustography[J].International Journal of Fatigue,2002,24(2/3/4):257-261. [14] SHAHZAD A.Impact and fatigue properties of hempglass fiber hybrid biocomposites[J].Journal of Reinforced Plastics and Composites,2011,30(16):1389-1398. [15] GARNIER C,PASTOR M L,LORRAIN B.Fatigue behavior of impacted composite structures[J].Composite Structures,2013,100(5):443-450. [16] NIXONPEARSON O J,HALLETT S R,WITHERS P J,et al.Damage development in openhole composite specimens in fatigue:Part 1 experimental investigation[J].Composite Structures,2013,106(12):882-889. [17] UDA N,ONO K,KUNOOK.Compression fatigue failure of CFRP laminates with impact damage[J].Composite Science and Technology,2009,69(14):2308-2314. [18] KOO J M,CHOI J H,SEOK C S.Evaluation for residual strength and fatigue characteristics after impact in CFRP composites[J].Composite Structures,2013,105(8):58-65. [19] HOSOI A,SATO N,KUSUMOTO Y,et al.Highcycle fatigue characteristics of quasiisotropic CFRP laminates over 108 cycles:initiation and propagation of delamination considering interaction with transverse cracks[J].International Journal of Fatigue,2010,32(1):29-36. [20] American Society for Testing and Materials.D7136/D7136M12 Standard test method for measuring the damage resistance of a fiberreinforced polymer matrix composite to a dropweight impact event[S].[S.l.]:ASTM,2012:1-10. [21] 徐颖.复合材料层合板冲击损伤及冲击后疲劳寿命研究[D].南京:南京航空航天大学,2007.XU Ying.Research on impact damage of laminates and fatigue life of impacted laminates[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2007.(in Chinese) [22] 朱炜垚,许希武.复合材料层合板低速冲击后压压疲劳试验研究及寿命预报[J].工程力学,2013,30(5):412-414.ZHU Weiyao,XU Xiwu.Experiment research and fatigue life prediction of lowvelocityimpacted laminate under compressivecompressive fatigue load[J].Engineering Mechanics,2013,30(3):412-414.(in Chinese) [23] TONG Y,ISAACD H.Combined impact and fatigue of glass fiber reinforced composites[J].Composites:Part B Engineering,2008,39(3):505-512. [24] KOSMANN N,RIECKEN B T,SCHMUTZLER H,et al.Evaluation of a critical impact energy in GFRP under fatigue loading[J].Composite Science and Technology,2014,102(4):28-34. [25] 杨光松.损伤力学与复合材料损伤[M].北京:国防工业出版社出版,1995:119-121. [26] MITROVICA M,HAHN H T,CARMAN G P,et al.Effect of loading parameters on the fatigue behavior of impact damaged composite laminates[J].Composite Science and Technology,1999,59(14):2059-2078.
点击查看大图
计量
- 文章访问数: 639
- HTML浏览量: 4
- PDF量: 551
- 被引次数: 0