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基于能量耗散率的 NEPE 推进剂疲劳损伤分析

郭坚 许进升 高艳宾 何勇 陈雄

弹道学报2016,Vol.28Issue(2):62-67,6.
弹道学报2016,Vol.28Issue(2):62-67,6.

基于能量耗散率的 NEPE 推进剂疲劳损伤分析

Fatigue Damage Evaluation of NEPE Propellant Based on Dissipated Energy

郭坚 1许进升 1高艳宾 2何勇 1陈雄1

作者信息

  • 1. 南京理工大学机械工程学院,南京210094
  • 2. 中国兵器工业第208研究所,北京102202
  • 折叠

摘要

Abstract

To study the fatigue damage evolution of NEPE propellant in controlled strain fatigue tests ,the ratio of dissipated energy change-approach based on the distribution of dissipated energy was used to analyze the fatigue damage process .According to four strain-amplitudes,the uniaxial drawing fatigue test was conducted .The fatigue life and dissipated energy under different strain-amplitudes were obtained .The result shows that the energy approach can intuitively explain the damage accumulation in the process of fatigue damage.Plotting plateau value of ratio of dissipated-energy and fatigue life behave in a linear relation.The plateau value is highly dependent on the initial loading strain amplitude , and the plateau value increases with the strain amplitude .The accumulative rates of the damage increase with the strain levels for the adjacent loading cycles , but the fatigue life decreases relatively , and the mechanism of damage increasing between the adjacent loading cycles can be explained .

关键词

NEPE推进剂/耗散能/疲劳损伤/能量耗散变化比

Key words

NEPE propellant/dissipated energy/fatigue damage/ratio of dissipated energy change

分类

航空航天

引用本文复制引用

郭坚,许进升,高艳宾,何勇,陈雄..基于能量耗散率的 NEPE 推进剂疲劳损伤分析[J].弹道学报,2016,28(2):62-67,6.

基金项目

江苏省青年基金项目(BK20140772);中央高校基本科研业务费专项资金资助 ()

弹道学报

OA北大核心CSCDCSTPCD

1004-499X

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