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Equivalent Crack Approach for Predicting Fatigue Life of Pre-corroded Aluminum Alloys in Helicopter
邓景辉 陈平剑 付裕
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 0, (): 0 -0 .  DOI: 10.7527/S1000-6893.2017.221421

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341