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RESEARCH ON VIBRATION ENVIRONMENT TEST TECHNOLOGY OF AIRCRAFT STRUCTURE COMBINED WITH FATIGUE OR STATIC LOAD
Cao Qi;Shao Chuang;Yao Qihang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1998, (4): 405 -409 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341