留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于Hopkinson技术的CMDB推进剂动态起裂韧性实验

郑健 汪文强 陈雄 周长省 许进升

郑健, 汪文强, 陈雄, 周长省, 许进升. 基于Hopkinson技术的CMDB推进剂动态起裂韧性实验[J]. 航空动力学报, 2016, 31(10): 2522-2529. doi: 10.13224/j.cnki.jasp.2016.10.028
引用本文: 郑健, 汪文强, 陈雄, 周长省, 许进升. 基于Hopkinson技术的CMDB推进剂动态起裂韧性实验[J]. 航空动力学报, 2016, 31(10): 2522-2529. doi: 10.13224/j.cnki.jasp.2016.10.028
ZHENG Jian, WANG Wen-qiang, CHEN Xiong, ZHOU Chang-sheng, XU Jin-sheng. Experiment on dynamic fracture initiation toughness of CMDB propellant based on Hopkinson technology[J]. Journal of Aerospace Power, 2016, 31(10): 2522-2529. doi: 10.13224/j.cnki.jasp.2016.10.028
Citation: ZHENG Jian, WANG Wen-qiang, CHEN Xiong, ZHOU Chang-sheng, XU Jin-sheng. Experiment on dynamic fracture initiation toughness of CMDB propellant based on Hopkinson technology[J]. Journal of Aerospace Power, 2016, 31(10): 2522-2529. doi: 10.13224/j.cnki.jasp.2016.10.028

基于Hopkinson技术的CMDB推进剂动态起裂韧性实验

doi: 10.13224/j.cnki.jasp.2016.10.028
基金项目: 

预研项目(20101019)

详细信息
    作者简介:

    郑健(1978-)男,浙江台州人,副教授,博士,主要研究方向为固体火箭发动机总体技术.E-mail:zhengjian@njust.edu.cn

  • 中图分类号: V435

Experiment on dynamic fracture initiation toughness of CMDB propellant based on Hopkinson technology

  • 摘要: 为了研究改性双基(CMDB)推进剂的动态起裂韧性,利用Hopkinson实验技术对CMDB推进剂的含切缝半圆形(NSCB)试件进行了冲击实验.运用脉冲整形技术,获得了CMDB推进剂的载荷-位移曲线.采用改进型柔度变化率法得到NSCB推进剂试件的起裂点.通过ABAQUS有限元软件对NSCB试件的无量纲结构因子进行了标定,并获得了NSCB的动态起裂韧性.利用电镜扫描设备分析了NSCB试件断裂的微观机理,研究结果表明:在加载率为5.41×105~8.94×105MPa·m1/2·s-1范围内,CMDB推进剂的动态起裂韧性具有显著的加载率敏感性.结合电镜扫描图分析,随着加载率的增大,断面内部颗粒微观结构的破坏形貌逐渐恶化,消耗的能量相应增大.

     

  • [1] Smith C W,Liu C T.Effects of near-tip behavior of particulate composites on classical concepts[J].Composites Engineering,1991,1(4):249-257.
    [2] Liu C T.Crack growth behavior in a solid propellant[J].Engineering Fracture Mechanics,1997,56(1):127-135.
    [3] Tussiwand G S,Saouma V,Terzenbach R,et al.Fracture mechanics of composite solid rocket propellant grains:material testing[J].Journal of Propulsion and Power,2009,25(1):60-73.
    [4] Knauss W G.Fracture and failure at and near interfaces under pressure[R].California:California Institute of Technology Pasadena Graduate Aeronautical Labs,ADA348939,1998.
    [5] Ho S Y,Fong C W.Temperature dependence of high strain-rate impact fracture behavior in highly filled polymeric composite and plasticized thermoplastic propellants[J].Journal of Materials Science,1987,22(8):3023-3031.
    [6] 刘朝丰,陈飞,阳建红.固体推进剂断裂韧性试验方法研究[J].宇航学报,2007,27(增刊1):186-189. LIU Chaofeng,CHEN Fei,YANG Jianhong.Test method research on solid propellant fracture toughness[J].Journal of Astronautics,2007,27(Suppl.1):186-189.(in Chinese)
    [7] 韩波,鞠玉涛,周长省.HTPB 推进剂粘聚区本构模型反演识别研究[J].兵工学报,2012,33(11):1335-1341. HAN Bo,JU Yutao,ZHOU Changsheng.Inversion identification of constitutive model of cohesive zone in HTPB propellant[J].Acta Armamentarii,2012,33(11):1335-1341.(in Chinese)
    [8] 韩波,鞠玉涛,周长省.HTPB 推进剂粘聚断裂研究[J].固体火箭技术,2013,36(1):89-93. HAN Bo,JU Yutao,ZHOU Changsheng.Cohesive fracture investigation of HTPB propellant[J].Journal of Solid Rocket Technology,2013,36(1):89-93.(in Chinese)
    [9] 胡少青,鞠玉涛,韦震,等.双基推进剂的切口强度及切口敏感性[J].航空动力学报,2014,29(8):2012-2016. HU Shaoqing,JU Yutao,WEI Zhen,et al.Notch strength and notch sensitivity of double base propellant[J].Journal of Aerospace Power,2014,29(8):2012-2016.(in Chinese)
    [10] 汪文强,郑健,陈雄,等.基于扩展有限元的改性双基推进剂的开裂过程模拟研究[J].推进技术,2015,36(1):149-155. WANG Wenqiang,ZHENG Jian,CHEN Xiong,et al.Numerical simulation of crack propagation in CMDB propellant based on extended finite element method[J].Journal of Propulsion Technology,2015,36(1):149-155.(in Chinese)
    [11] Zhang Q B,Zhao J.Determination of mechanical properties and full-field strain measurements of rock material under dynamic loads[J].International Journal of Rock Mechanics and Mining Sciences,2013,60:423-439.
    [12] Wang Q Z,Feng F,Ni M,et al.Measurement of mode Ⅰ and mode Ⅱ rock dynamic fracture toughness with cracked straight through flattened Brazilian disc impacted by split Hopkinson pressure bar[J].Engineering Fracture Mechanics,2011,78(12):2455-2469.
    [13] Foster J T,Chen W,Luk V K.Dynamic crack initiation toughness of 4340 steel at constant loading rates[J].Engineering Fracture Mechanics,2011,78(6):1264-1276.
    [14] 陈荣.一种 PBX 炸药试样在复杂应力动态加载下的力学性能实验研究[D].长沙:国防科学技术大学,2010. CHEN Rong.Experimental studies on mechanical properties of a PBX under various dynamic loading conditions[D].Changsha:National University of Defense Technology,2010.(in Chinese)
    [15] Kobayashi T,Yamamoto I,Niinomi M.Introduction of a new dynamic fracture toughness evaluation system[J].Journal of Testing and Evaluation,1993,21(3):145-153.
    [16] Zhang Q B,Zhao J.Effect of loading rate on fracture toughness and failure micro-mechanisms in marble[J].Engineering Fracture Mechanics,2013,102(2):288-309.
    [17] Chong K P,Kuruppu M D.New specimen for fracture toughness determination for rock and other materials[J].International Journal of Fracture,1984,26(2):59-62.
    [18] Lim I L,Johnston I W,Choi S K.Stress intensity factors for semi-circular specimens under three-point bending[J].Engineering Fracture Mechanics,1993,44(3):363-382.
  • 加载中
计量
  • 文章访问数:  892
  • HTML浏览量:  1
  • PDF量:  466
  • 被引次数: 0
出版历程
  • 收稿日期:  2015-01-21
  • 刊出日期:  2016-10-28

目录

    /

    返回文章
    返回