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Finite Element Method for Structure Analysis of Filamentwound  Composite Based on Micro Stiffness Model
Li Jian;Wen Weidong;Cui Haitao;Xu Ying
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2009, (7): 1236 -1242 . 

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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