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基于临界面法及应变路径多轴疲劳寿命预测模型概述

Translated title of the contribution: Research on multi axis low cycle fatigue life prediction models based on critical plane method and strain path
  • Hongbin Liu*
  • , Wei Chen
  • , Yanrong Wang
  • *Corresponding author for this work
  • Nanjing University of Aeronautics and Astronautics
  • Aero Engine Corporation of China

Research output: Contribution to journalArticlepeer-review

Abstract

The article has done some research on multiaxial low cycle fatigue life evaluation methods at home and abroad, summarized multiaxial low cycle fatigue life prediction models based on Critical-Plane method and strain path and analyzed the advantages and disadvantages compared with models and applicability. It has been shown that most of the empirical prediction methods could suitable for only one or few materials so far. When they are applied on other materials, the results are usually disappointing. Meanwhile, the multi-axial fatigue failure of materials are very complicated. The current massive research work was mainly done under constant temperature and load while the studies carried out on high temperature, varying temperature and load are few. If taking notch effect, size effect, surface roughness, residual stress into account, the situation would be even more complicated. Current research on multi axis fatigue is interested in establishing life prediction model, To carry out related fatigue test,Little in-depth study of its micro mechanism The multi-axial fatigue is still a problem needing further studies.

Translated title of the contributionResearch on multi axis low cycle fatigue life prediction models based on critical plane method and strain path
Original languageChinese (Traditional)
Pages (from-to)173-180
Number of pages8
JournalJixie Qiangdu/Journal of Mechanical Strength
Volume41
Issue number1
DOIs
StatePublished - 15 Feb 2019

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