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Structural Dynamic Optimization for Flexible Beam of Helicopter Rotor Based on GA

GAO Yadong PI Runge HUANG Dawei

南京航空航天大学学报：英文版2022，Vol.39Issue(6)：P.721-734,14.

南京航空航天大学学报：英文版2022，Vol.39Issue(6)：P.721-734,14.DOI:10.16356/j.1005-1120.2022.06.008

Structural Dynamic Optimization for Flexible Beam of Helicopter Rotor Based on GA

GAO Yadong ¹PI Runge ²HUANG Dawei¹

作者信息

1. National Key Laboratory of Rotorcraft Aeromechanics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China
2. National Key Laboratory of Rotorcraft Aeromechanics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China Equipment Department,China Aero-Polytechnology Establishment,Beijing 100028,P.R.China
折叠

摘要

关键词

bearing-less rotor system/flexible beam/dynamic optimization/Hamilton variational principle/variational asymptopic beam section analysis/genetic algorithm(GA)

分类

通用工业技术

引用本文复制引用

GAO Yadong,PI Runge,HUANG Dawei..Structural Dynamic Optimization for Flexible Beam of Helicopter Rotor Based on GA[J].南京航空航天大学学报：英文版,2022,39(6):P.721-734,14.

基金项目

supported by the Foundation of National Key Laboratory of Rotorcraft Aeromechanics,Nanjing University of Aeronautics and Astronautics(No.614222004030917)。（No.614222004030917）

南京航空航天大学学报：英文版

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ISSN：1005-1120

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