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Prediction of Delamination Threshold Load for Impact on Composite Laminate Based on Modified Interlaminar Shear Strength Criterion
GAO Shangjun, YU Zhefeng, WANG Hai
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2014, (5): 1329 -1335 .  DOI: 10.7527/S1000-6893.2013.0512

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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