... lift dissymmetry 升力不对称 lift distribution 升力分布 lift distribution; across span 翼展向升力分布 ...
基于13个网页-相关网页
椭圆升力分布 lift distribution ; elliptic
翼展向升力分布 lift distribution ; across span
弦向升力分布 chordwise lift distribution ; lift distribution ; chord-wise
展向升力分布 spanwise lift distribution ; lift distribution ; span-wise
椭圆升力分布机翼 elliptical lift distribution wing
机翼升力分布 wing lift distribution
前后升力分布 fore-and-aft lift distribution
机身升力分布 fuselage lift distribution
升力重新分布 lift redistribution
At the end of this article, a surrogate model is created to describe the lift distribution of a wing.
并且通过构造描述机翼展向升力分布的代理模型，对上述几种方法作了对比分析。
参考来源 - 多学科设计优化代理模型技术的研究和应用·2,447,543篇论文数据，部分数据来源于NoteExpress
可以用它来计算亚音速时弹性飞机的升力分布及11个主要的纵向气动导数。
This method can be used to evaluate the lift distribution and 11 main longitudinal aerodynamic derivatives of elastic aircraft at subsonic speeds.
本文提供了一种根据升力面理论计算螺旋桨桨叶表面压力分布和螺旋桨性能的数值方法。
A numerical method is presented for prediction of propeller performance and pressure distribution on blade surface according to lifting surface theory.
压强分布和升力系数的计算值与现存文献的数值结果和实验数据是一致的。
Predicted pressure distribution and lift coefficient are in agreement with numerical results and experimental data available in the literature.
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