南京航空航天大学主页平台管理系统尚丽娜--中文主页-- Geometrically exact aeroelastic stability analysis of composite helicopter rotor blades in hover by updated VABS

Geometrically exact aeroelastic stability analysis of composite helicopter rotor blades in hover by updated VABS: 点击次数：; 发布时间： 2024-02-22; 所属单位：航空学院; 发表刊物：Journal of Aerospace Engineering; 论文类型：期刊论文; 是否译文：否; 发表时间：2023-11-29; 收录刊物：SCI; 第一作者：Shang Lina; 通讯作者：Xia Pinqi

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