In this paper, an effective design optimization method for High-aspect-ratio composite wing skin is presented.
论文以大展弦比飞翼布局机翼蒙皮的优化设计为背景，开展了复合材料层压板结构的优化设计工作。
2
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。
3
Most part of the supercritical wing with equal chord and highaspectratio is provided with 2-D flow characteristics approximately except wing tip.