A model-based prognostics method for fatigue crack growth in fuselage panels
accepted 27 March 2018Available online 7 January 2019* Corresponding author.Peer review under responsibility of Editorial Committee of CJA.
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The present work was partially funded by the National Natural Science Foundation of China 51805262
2019-09-27(万方平台首次上网日期,不代表论文的发表时间)
共13页
396-408