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1)  Flying wing with high aspect-ratio
大展弦比飞翼结构
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 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。
4)  high aspect ratio wing
大展弦比机翼
1.
With the issue that structural nonlinearity has great effect on dynamic characteristics of high aspect ratio wing,the finite element modeling is built for high aspect ratio composite wing by using MSC Patran and Nastran,which is modeled as a thin-walled box beam.
针对结构非线性对大展弦比机翼动力学特性影响很大的问题,使用MSC Patran和MSC Nastran软件进行有限元建模及分析,将大展弦比机翼建成薄壁盒型梁模型。
5)  high-aspect-ratio wing
大展弦比机翼
1.
Influence of chordwise bending stiffness on aeroelastic characteristics of flexible high-aspect-ratio wing
水平弯曲刚度对大展弦比机翼颤振的影响
6)  large aspect ratio wing
大展弦比机翼
1.
Aeroelastic phenomena are significant for high-altitude long-endurance aircrafts for the large aspect ratio wing.
高空长航时飞机普遍具有大展弦比机翼 ,其气动弹性问题尤为突出 。
补充资料:毋翼而飞
1.比喻传播之迅速。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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