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仿生折叠翼扑动过程气动特性分析

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以甲虫后翅为仿生对象,基于四板机构理论设计了一种仿甲虫四板折叠翼,并对其气动特性进行研究.建立了仿甲虫四板折叠翼动力学仿真模型,采用双向流固耦合数值模拟方法,分析了扑动幅值、拍动频率与前飞速度对柔性折叠翼的升阻力系数和空气流场的影响,并对柔性折叠翼扑动过程进行了流场研究.研究表明,柔性折叠翼能提高飞行器的升力特性和推力特性,其扑动幅值为80°,频率为50Hz时,折叠翼的气动特性最为显著.本研究工作为优化折叠翼的设计及控制奠定了基础.
Analysis of Aerodynamic Characteristics of Bionic Folding Wing During Flapping
Taking the beetle hind wings as a bionic object,a four-plate folding wing like the beetle was designed based on the theory of four-plate mechanism,and its aerodynamic characteristics were studied.A dynamic simulation model of the beetle-like four-plate folding wing was established.Using a two-way fluid-structure coupling numerical simulation method,the effects of flapping amplitude,flapping frequency and forward flight speed on the lift-drag coefficient and air flow field of the flexible fold-ing wing were analyzed.The fluttering process of the flexible folding wing is studied in the flow field.Studies have shown that flex-ible folding wings can improve the lift characteristics and thrust characteristics of the aircraft.When the flapping amplitude is 80° and the frequency is 50Hz,the aerodynamic characteristics of the folding wings are the most significant.This research work laid the foundation for optimizing the design and control of the folding wing.

Folding WingFlexible Flapping WingFluid-Structure CouplingAerodynamic Characteristics

王才东、张昊田、胡坤、王新杰

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郑州轻工业大学机电工程学院,河南 郑州 450002

折叠翼 柔性扑翼 流固耦合 气动特性

国家自然科学基金

51705473

2024

机械设计与制造
辽宁省机械研究院

机械设计与制造

CSTPCD北大核心
影响因子:0.511
ISSN:1001-3997
年,卷(期):2024.398(4)
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