Fatigue crack growth simulation in a first stage of compressor blade
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Materials Science
Reference24 articles.
1. Fracture analysis of compressor blade of a helicopter engine;Witek;Eng Fail Anal,2009
2. Influence of coatings obtained by PVD on the properties of aircraft compressor blades;Swadzba;Surf Coat Technol,1996
3. Fatigue strength and life of compressor blades for marine gas turbine engines;Troshchenko;Strength Mater,1999
4. Experimental crack propagation and failure analysis of the first stage compressor blade subjected to vibration;Witek;Eng Fail Anal,2009
5. Interacting dissimilar semi-elliptical surface flaws under tension and bending;Murakami;Eng Fract Mech,1982
Cited by 47 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. Crack Evaluation Using Deep Learning Model for Prediction of Stress Intensity Factor of Aircraft Structure;Journal of the Korean Society for Aeronautical & Space Sciences;2024-09-30
2. Formation mechanism of blade surface integrity based on hybrid process of cryogenic minimum quantity lubrication and ultrasonic rolling strengthening process;Materials & Design;2024-09
3. Failure investigation of fatigue crack initiation and propagation in compressor blade;Engineering Failure Analysis;2024-08
4. Support vector regression-assisted finite element method for mode I-II fatigue crack growth path prediction;Theoretical and Applied Fracture Mechanics;2024-06
5. Peridynamics-based analysis on fracture behaviors of a turbine blade shroud;Engineering Fracture Mechanics;2024-01
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3