A Crack-Closure Model for Predicting Fatigue Crack Growth under Aircraft Spectrum Loading-Reference-Cited by-同舟云学术

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A Crack-Closure Model for Predicting Fatigue Crack Growth under Aircraft Spectrum Loading

Published: Issue: Volume: Page:53-53-32
ISSN:
Container-title:Methods and Models for Predicting Fatigue Crack Growth Under Random Loading
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Author:

Newman JC

Publisher

ASTM International

Cited by 248 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. Equations for efficient cycle-by-cycle computation of fatigue crack retardation and acceleration due to amplitude changes;Theoretical and Applied Fracture Mechanics;2024-10

2. Fatigue crack extension mechanism and mode-type analyses of martensitic steels for proposing fatigue strength evaluation method: Example of 18% Ni BCC martensitic steel;Theoretical and Applied Fracture Mechanics;2024-10

3. Determination of cyclic R-curve for predicting short fatigue crack growth;Theoretical and Applied Fracture Mechanics;2024-10

4. Efficient technique for evaluation of three-dimensional elastic–plastic fracture mechanics parameters based on equivalent distributed stress concept;Theoretical and Applied Fracture Mechanics;2024-06

5. Fatigue crack growth behavior of a nickel-based superalloy under turbine standard spectrum loads;International Journal of Fracture;2024-05-17

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