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Nonlinear Aeroelastic Coupled Trim Analysis of a Twin Cyclocopter in Forward Flight
AIAA Journal ( IF 2.5 ) Pub Date : 2021-01-01 , DOI: 10.2514/1.j059122
Atanu Halder 1 , Moble Benedict 1
Affiliation  

The paper discusses the development of a nonlinear aeroelastic coupled trim model of a twin cyclocopter in forward flight. The twin cyclocopter consists of two cycloidal rotors as main thrusters an...

中文翻译:

双旋翼机前飞非线性气动弹性耦合配平分析

本文讨论了前飞双旋翼飞行器非线性气动弹性耦合配平模型的开发。双旋翼飞行器由两个摆线转子作为主推进器和...
更新日期:2021-01-01
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