In this paper, an approximate method is presented to compute low-speed aerodynamic characteristics of high-middle aspectratio and low sweep Angle wing with separation.
本文介绍一种计算带分离的大中层弦比、小后掠角机翼低速气动特性的近似方法。
2
The aerodynamic characteristics of low Reynolds number, the influence of separation bubble and aspectratio are discussed.
讨论了低雷诺数空气动力特性,包括分离气泡和展弦比的影响。
3
The aerodynamic computation and the design of optimized wing sails for aircraft with rectangular wing whose aspectratio equals 8. 6 were completed.