Critical crack tip opening displacement (CTODc) of concrete using experimental and analytical evaluation with seven different compressive strengths ranging from 30 up to 150 MPa was studied based on two types of fract...Critical crack tip opening displacement (CTODc) of concrete using experimental and analytical evaluation with seven different compressive strengths ranging from 30 up to 150 MPa was studied based on two types of fracture tests:three-point bending (TPB) and wedge splitting (WS).In the tests,the values of CTODc were experimentally recorded using a novel technique,in which fiber Bragg grating (FBG) sensors were used,and two traditional techniques,in which strain gauges and clip gauges were deployed.The values of CTODc of tested concrete were also predicted using two existing analytical formulae proposed by JENQ & SHAH and XU,respectively.It is found that the values of CTODc obtained by both experimental measurements and analytical formulae exhibit a negligible variation as the compressive strength of concrete increases,and the test geometry adopted has little impact on the value of CTODc.Regarding the experimental measurement of CTODc,the clip gauge method generally leads to a larger value of CTODc and shows a more significant scatter as compared with the other two methods,while the strain gauge method leads to a slightly lower CTODc as compared with the FBG sensor method.The analytical formula proposed by JENQ and SHAH is found to generally lead to an overestimation,while the analytical formula proposed by XU shows a good accuracy.展开更多
老龄飞机中由于多裂纹的产生将导致结构剩余寿命大幅削减。针对如飞机机舱上布有沿纵向铆钉接头的隔板结构,文中给出一种分析多部位损伤结构剩余强度的方法。裂纹扩展模型是分析的基础,文中对两类(单参量和三参量)扩展模型进行讨论,给...老龄飞机中由于多裂纹的产生将导致结构剩余寿命大幅削减。针对如飞机机舱上布有沿纵向铆钉接头的隔板结构,文中给出一种分析多部位损伤结构剩余强度的方法。裂纹扩展模型是分析的基础,文中对两类(单参量和三参量)扩展模型进行讨论,给出裂纹在增量载荷下萌生与稳定扩展的处理方法。基于Irwin和Dugdale裂尖张开位移模型与Swift准则,给出较为完整的分析多部位损伤(multiple site damage,MSD)结构剩余强度的方法。最后,通过对飞机压力舱上的沿纵向铆钉接头的模拟计算,对文中方法进行验证。由分析结果可知,采用文中方法计算得到的剩余强度值与试验值符合得较好,该方法能较为准确有效地对复杂MSD结构的剩余强度进行分析。展开更多
基金Project(50438010) supported by the Key Program of the National Natural Science Foundation of ChinaProject(JGZXJJ2006-13) supported by the Research and Application Programs of Key Technologies for Major Constructions in the South-North Water Transfer Project Construction in China
文摘Critical crack tip opening displacement (CTODc) of concrete using experimental and analytical evaluation with seven different compressive strengths ranging from 30 up to 150 MPa was studied based on two types of fracture tests:three-point bending (TPB) and wedge splitting (WS).In the tests,the values of CTODc were experimentally recorded using a novel technique,in which fiber Bragg grating (FBG) sensors were used,and two traditional techniques,in which strain gauges and clip gauges were deployed.The values of CTODc of tested concrete were also predicted using two existing analytical formulae proposed by JENQ & SHAH and XU,respectively.It is found that the values of CTODc obtained by both experimental measurements and analytical formulae exhibit a negligible variation as the compressive strength of concrete increases,and the test geometry adopted has little impact on the value of CTODc.Regarding the experimental measurement of CTODc,the clip gauge method generally leads to a larger value of CTODc and shows a more significant scatter as compared with the other two methods,while the strain gauge method leads to a slightly lower CTODc as compared with the FBG sensor method.The analytical formula proposed by JENQ and SHAH is found to generally lead to an overestimation,while the analytical formula proposed by XU shows a good accuracy.
文摘老龄飞机中由于多裂纹的产生将导致结构剩余寿命大幅削减。针对如飞机机舱上布有沿纵向铆钉接头的隔板结构,文中给出一种分析多部位损伤结构剩余强度的方法。裂纹扩展模型是分析的基础,文中对两类(单参量和三参量)扩展模型进行讨论,给出裂纹在增量载荷下萌生与稳定扩展的处理方法。基于Irwin和Dugdale裂尖张开位移模型与Swift准则,给出较为完整的分析多部位损伤(multiple site damage,MSD)结构剩余强度的方法。最后,通过对飞机压力舱上的沿纵向铆钉接头的模拟计算,对文中方法进行验证。由分析结果可知,采用文中方法计算得到的剩余强度值与试验值符合得较好,该方法能较为准确有效地对复杂MSD结构的剩余强度进行分析。