Composite material wing structure optimization method based on topological optimization
The invention discloses a composite material wing structure optimization method based on topological optimization, and the method comprises the steps: carrying out the preliminary optimization through employing a topological optimization method based on a finite element model of a target structure,...
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Main Authors | , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
26.01.2024
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Subjects | |
Online Access | Get full text |
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