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IMPROVEMENTS IN TEST METHOD FOR FATIGUE THRESHOLDS AND LOW FATIGUE CRACK GROWTH RATE
Ding Chuanfu;Zhao Wei;Gu Mingda
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1987, (2): 115 -118 . 

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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