Aircraft duraluminum wing spar fatigue testing-Reference-Cited by-同舟云学术

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Aircraft duraluminum wing spar fatigue testing

Published:2017 Issue:4 Volume:45 Page:531-536
ISSN:1451-2092
Container-title:FME Transaction
language:en
Short-container-title:FME Transaction

Author:

Petrasinovic Nikola,Petrasinovic Danilo,Rasuo Bosko,Milkovic Dragan

Publisher

Centre for Evaluation in Education and Science (CEON/CEES)

Subject

Mechanical Engineering,Mechanics of Materials

Link

https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2017/1451-20921704531P.pdf

Cited by 30 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

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2. Fatigue life prediction of AA2524 thin plate strengthened using compound laser heating and laser shot peening method;Theoretical and Applied Fracture Mechanics;2024-02

3. A novel shock life model for BGA solder joints based on evolutionary power spectral density;International Journal of Fatigue;2023-10

4. Fatigue damage diagnosis and prognosis for 2024 aluminum plates with center holes: A strain monitoring approach;International Journal of Fatigue;2023-05

5. Vibration fatigue performance improvement in 2024-T351 aluminum alloy by ultrasonic-assisted laser shock peening;International Journal of Fatigue;2023-03

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