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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Compilation and indexing terms; Copyright 2024 Elsevier Inc;
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摘要：
Stringers - Orthotropic plates - Wings
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