New-Trim-Method-Based Investigation on the Cyclic-Pitch-Effected Advancing-Blade-Concept Helicopter Aerodynamics

Lyu Wei-Liang; Xu Guo-Hua

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New-Trim-Method-Based Investigation on the Cyclic-Pitch-Effected Advancing-Blade-Concept Helicopter Aerodynamics

机译：基于新方法的螺旋桨推进概念的循环桨距空气动力学研究

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来源
《Journal of Aircraft》 |2015年第4期|1365-1371|共7页
作者
Lyu Wei-Liang; Xu Guo-Hua;
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作者单位

Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Sch Aeronaut & Astronaut, Dalian 116024, Peoples R China;

Nanjing Univ Aeronaut & Astronaut, Natl Key Lab Rotorcraft Aeromech, Sch Aeronaut & Astronaut, Nanjing 210016, Peoples R China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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New-Trim-Method-Based Investigation on the Cyclic-Pitch-Effected Advancing-Blade-Concept Helicopter Aerodynamics

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