Fatigue life prediction of aircraft structures—past, present and future-Reference-Cited by-同舟云学术

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Fatigue life prediction of aircraft structures—past, present and future

Published:1974-12 Issue:4 Volume:6 Page:745-762
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Schütz Walter

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference84 articles.

1. A comparison of predicted and achieved fatigue lives of aircraft structures;Raithby,1971

2. The U.S. Air Force weapon systems fatigue certification program;Lowndes,1965

3. The value of full scale testing;Harpur,1965

4. Correlation between full scale fatigue test and service experience;Lowndes,1969

5. Correlation between test and service experience;Troughton,1969

Cited by 11 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. Fatigue Life and Crack Growth Rate Prediction of Additively Manufactured 17-4 PH Stainless Steel using Machine Learning;Procedia Structural Integrity;2024

2. A review on the fatigue behaviour of AlSi10Mg alloy fabricated using laser powder bed fusion technique;Journal of Materials Research and Technology;2022-03

3. Prediction of Fatigue Crack Growth Behaviour in Ultrafine Grained Al 2014 Alloy Using Machine Learning;Metals;2020-10-09

4. Developing an accelerated flight load spectrum based on the n-N curves of a fleet;International Journal of Fatigue;2018-12

5. Bibliography;Fatigue Damage;2014-04-11

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