1) low-aspect-ratio wing
小展弦比机翼
1.
Based on the time-derivative proconditioned method,the low speed aerodynamic propertics of low-aspect-ratio wing are numerically simulated.
以雷诺平均的Navier-Stokes方程为基础,应用非结构混合网格技术,基于有限体积的时间推进预处理方法,对小展弦比机翼的低速流动进行了数值模拟。
2.
To investigate viscous flows around low-aspect-ratio wings of a micro-aerial vehicle(MAV) at low Reynolds numbers,experiments are conducted in a wind tunnel using particle image velocimetry(PIV) and a smoke wire technique.
应用粒子图像速度场仪(PIV)和烟线两种流动显示技术,测量低雷诺数下小展弦比机翼粘性绕流的流场。
2) low-aspect wing
小展弦比机翼<火>
3) vanishing aspect ratio airfoil
无限小展弦比机翼
4) stub wing
小展弦和收缩比机翼<火>
5) LAR (low aspect ratio)
(叶片或机翼)小展弦比
6) low aspect ratio flying wing
小展弦比飞翼
1.
Vortex control in low aspect ratio flying wing;
涡流控制在小展弦比飞翼布局飞机上的应用研究
2.
In order to improve the lateral control ability of the low aspect ratio flying wing aircraft, a vortex control method is designed which can provide rolling moment for the aircraft, and the effects of leading dissymmetrical vertical injects on flow structure are studied.
为增加小展弦比飞翼布局飞机横向控制效能,设计了可提供飞机滚转力矩的涡流控制方案,在此基础上研究了三角翼前缘非对称垂直喷流对前缘涡破裂位置和结构的影响。
3.
Neural network control in active vortex control based on low aspect ratio flying wing;
以小展弦比飞翼布局飞机为研究对象,其本体的优化增稳控制器由3个气动舵面(连续控制面)构成。
补充资料:齐展展
1.整整齐齐。
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