Fatigue life retro estimation of wing structure under different load spectra-Reference-Cited by-同舟云学术

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Fatigue life retro estimation of wing structure under different load spectra

Published:2004-08 Issue:4 Volume:11 Page:605-612
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Zhang Weifang,Li Yunju,Liu Gaoyuan,Zhao Aiguo,Tao Chunhu

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference6 articles.

1. Analysis on metal fracture surface,1998

2. Practical analysis on mechanics failure,1997

3. Failure analysis and prevention for rotor in aero-engine,2000

4. Quantitative connection between macro morphology of metal fracture surface and mechanics parameter;Zhong;Enginery Materials and Mechanics,1984

5. Fatigue stress retro estimation study on fracture surface;Xie;Journal of Aeronautical Materials,2001

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Spectral-Based Fatigue Life Analysis of Bus Structural Steels with Different Nodes and Operating Tracks;ENG T-POL;2023

2. Study on test and preparation of load spectrum of hydraulic excavator;SPIE Proceedings;2017-01-23

3. Fatigue Propagation Life Evaluating for Materials or Components Suffered Load Spectrum by Quantitative Fractography;Advanced Materials Research;2014-02

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