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一种基于多体动力学的直升机复杂构型桨叶建模方法

Release Time:2026-03-13  Hits:

First Author: 彭海军

Disigner of the Invention: 王刚,宋宁宁,李飞

Institution: 力学与航空航天学院

Application Date: 2025-05-08

Application Number: CN202510586263.3

Authorization Date: 2025-09-09

Authorization Number: ZL202510586263.3

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