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STUDY ON MULTIAXIAL FATIGUE DAMAGE PARAMETERS BASED ON THE CRITICAL PLANE APPROACH
SHANG De guang;YAO Wei xing
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1999, (4): 8 -11 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341