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Nonlinear Aeroelastic Coupled Trim Analysis of a Twin Cyclocopter in Forward Flight
AIAA Journal ( IF 2.1 ) Pub Date : 2021-01-01 , DOI: 10.2514/1.j059122 Atanu Halder 1 , Moble Benedict 1
AIAA Journal ( IF 2.1 ) 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
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...