翼
后缘
机翼扭转
前沿
偏转(物理)
外倾角(空气动力学)
航空航天工程
机翼载荷
空气动力学
升力系数
结构工程
升阻比
工程类
攻角
物理
机械
光学
湍流
雷诺数
作者
Kang Li,Weitao Ba,Lei Yang,Shui-Yan Lv,Yang Yang,Lijun Xie
出处
期刊:Journal of physics
[IOP Publishing]
日期:2023-06-01
卷期号:2478 (10): 102037-102037
标识
DOI:10.1088/1742-6596/2478/10/102037
摘要
Abstract The trailing edge deformable wing is one of the main development directions of future aircraft design. The technology of active camber of wing trailing edge can significantly improve the aerodynamic performance of aircraft. In this paper, the motor drives the parabolic crankshaft and the distributed crankshaft drives the flexible skin of the trailing edge of the wing, which can realize the deflection of the trailing edge of the wing at a large angle of 0~30 degrees. At the same time, the surface of the wing is continuous and smooth. Moreover, the aerodynamic simulation results of the deformed wing show that the trailing edge deflection is beneficial to increase the lift. It can increase the maximum lift coefficient by 2 times and the maximum lift drag ratio by 18%. Adaptive flexible wing technology is applied to rocket sleds with side wings. This technology can increase the downward pressure of the side wing of the rocket block and improve the operation safety.
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