欢迎您！东篱公司
退出
-
申报数据库
-
立项数据库
-
成果数据库
-
项目获奖数据库
中文摘要：
为研究扑动飞行器悬停时扑翼的变形给气动力及周围流场带来的影响,通过求解二维Navier-Stokes方程,分析了扑翼气动力及其周围流场结构随扑翼柔性变形的变化规律.结果显示,当扑翼在悬停扑动时,适当的柔性变形可以提高升力,增大升阻比,有效地改善气动特性.但是,过度的柔性变形会使扑翼的气动特性恶化,升力和升阻比随着过度的变形而减小.
英文摘要：
By solving the two dimensional Navier-Stokes equations,a numerical study on the effect of flapping wing deformation on aerodynamic forces is carried out while the wing is in hovering flight,and the variations of aerodynamic forces and flow patterns around the flapping wing with the wing deformation are examined.The results show that the flapping wing provides a higher lift force when it is in an appropriate deformation and hence gives better aerodynamic performance than a rigid one.However,an excessive deformation of the wing may make the aerodynamic performance of the wing worse.
同期刊论文项目
同项目期刊论文
Numerical Investigation on the Aerodynamic characteristics of a Forward Flight Flapping Airfoil with
Observational analysis of asymmetric distribution of convection associated with tropical cyclone “ch
Characteristics of the offshore extreme wind load on parameters for wind turbines during strong typh
Atmospheric boundary layer characteristics over the Pearl River Delta, China, during the summer of 2
Numerical simulations of cross-flow around four square cylinders in an in-line rectangular configura
Bifurcation and chaos of a cable-beam coupled system under simultaneous internal and external resona
Simulation of flow past cable with upper rivulet on its surface and investigation of the cable dynam
Wind Speed Profile and Gradient Height in Typhoons Observed by Vehicular Doppler Radar in South Chin
期刊信息
位置：