A layout optimization method of composite wing structures based on carrying efficiency criterion

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作者：

Key Lab. of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China ^{[1
]}

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来源：

Chin J Aeronaut | / 4卷 / 425-433期

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摘要：

Stringers - Orthotropic plates - Wings

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