1) 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。
2) high aspect-ratio flying wing
大展弦比飞翼
1.
Integrate shape/size optimization into a high aspect-ratio flying wing design;
大展弦比飞翼结构形状、尺寸综合优化设计
3) 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。
4) low-aspect-ratio thin wings
小展弦比薄翼
1.
Analysis of wingtip vortex characteristics in flows around low-aspect-ratio thin wings for micro air vehicles;
微型飞行器小展弦比薄翼流场中的翼尖涡特性分析
2.
The three-dimensional incompressible Navier-Stokes equations are solved by artificial compressibility ap- proach,the flows around two kinds of low-aspect-ratio thin wings,flat and cambered,are simulated,numerical results a- gree well with the experimental data.
采用虚拟压缩方法求解三维不可压缩 N-S 方程,数值模拟了无弯度、有弯度两类微型飞行器低雷诺数小展弦比薄翼的流场,将得到的结果与实验进行了对比,数据间有较好的一致性。
5) low-aspect wing
小展弦比机翼<火>
6) low-aspect-ratio unswept wing
小展弦比平直翼
补充资料：双飞翼
1.喻指信使。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条