Computational study of aerodynamics of low aspect ratio wings
Aspect ratio (AR) and camber are studied numerically to have an insight into their effects on aerodynamic performance of micro air vehicles (MAV). Three-dimensional steady-state incompressible Navier-Stokes equations are solved numerically employing the artificial compressibility method. Results show that it is more beneficial to have a wing with an AR as high as possible while still within the design size and cambered wing yields more outstanding aerodynamic characteristics in MAV design.
MAV LAR low Reynolds number artificial compressibility formulation camber
J.Liu P.F.Weng
Shanghai University, Shanghai Institute of Applied Mathematics and Mechanics, Shanghai, 200072, China
国际会议
The Fifth International Conference on Fluid Mechanics(第五届国际流体力学会议)
上海
英文
2007-08-15（万方平台首次上网日期，不代表论文的发表时间）