The USAF characteristic K approach for cracks growing from small material discontinuities under combat aircraft and civil aircraft load spectra-Reference-Cited by-同舟云学术

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The USAF characteristic K approach for cracks growing from small material discontinuities under combat aircraft and civil aircraft load spectra

Published:2017-10 Issue: Volume:80 Page:39-48
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Huang Pu,Peng Daren,Jones Rhys^ORCID

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference23 articles.

1. Threats to Aircraft Structural Safety, Including a Compendium of Selected Structural Accidents/Incidents, ASC-TR-2010-5002;Tiffany,2010

2. Railwayage;Gonzales,2012

3. Fatigue crack growth and damage tolerance;Jones;Fatigue Fract. Eng. Mater. Struct.,2014

4. On the growth of fatigue cracks from corrosion pits and manufacturing defects under variable amplitude loading;Jones;JOM,2015

Cited by 7 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. USAF Characteristic K Approach: A Robust Tool for Predicting Fatigue Crack Growth under Various Underload Spectra;Materials;2024-07-04

2. A Building Block Approach to Sustainment and Durability Assessment: Experiment and Analysis;Comprehensive Structural Integrity;2023

3. A damage tolerance approach for structural integrity of truck trailers;Engineering Failure Analysis;2022-06

4. Additively manufactured Ti-6Al-4V replacement parts for military aircraft;International Journal of Fatigue;2019-07

5. When do small fatigue cracks propagate and when are they arrested?;Corrosion Reviews;2019-06-13

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