1.
APPLICATION OF THE MULTIPLIER PENALTY FUNCTION METHOD TO THE OPTIMUM DESIGN OF WING CONFIGURATIONS OF AEROSPACE VEHICLE
乘子罚函数法在航天飞机机翼外形优化设计中的应用
2.
The computed examples are given and the results are valuable for the selection of wing shape at the preliminary design stage.
计算结果表明，方法对初步设计阶段中航天飞机机翼外形的选择，有参考价值。
3.
Shape Parameter Optimization for Wing and Wingtip Based on RBF
基于径向基函数的机翼和翼梢小翼外形优化
4.
A Study on Two-level Optimization Approach for Aerodynamic Design of Wing Shape;
面向机翼气动外形优化的二级优化方法研究
5.
Our aircraft was a beautifully presented Second World War Boeing Stearman open cockpit biplane.
我们的飞机是一架外形美观的二战时的波音斯蒂尔曼敞座双翼机。
6.
An Effective Aerodynamic and Aeroelastic Coupled Design Method for Complicated Wing Shape
考虑气动弹性影响的机翼复杂气动外形设计研究
7.
The Joukowski airfoil problem is the simplest application of conformal mapping to airfoil design.
joukowski问题是最简单的翼型形映射应用到机翼设计.
8.
The inverse Zimmerman wing shows a better longitudinal stability and flow-field stability.
与矩形翼相比,反齐默曼机翼有较好的稳定性.
9.
Design of Flapping Mechanism for a Micro Air Vehicle Based on Mathematical Morphology;
基于数学形态学的微扑翼飞行器翅翼机构设计
10.
Study of the Wing Shape of Flapping-Wing MAV
扑翼飞行器机翼平面形状设计方法研究
11.
A Compliant Rib Based Morphing Wing Geometric Parameters Design
基于柔性翼肋的变形机翼几何参数设计
12.
Shape Optimization of Cruise Missile Based on the Concept of Telescopic Wing
伸缩弹翼巡航导弹气动外形优化研究
13.
delta wing (hang gliders)
三角形机翼（悬挂式滑翔机）
14.
Numerical Simulation of the Dynamic Aerodynamic Characteristics about Partial Flexible Airfoils and Folding Wing Aircraft
局部主动变形翼型和折叠翼变形飞机动态气动特性数值模拟研究
15.
Geometry Representation Method of Airfoil Based on Free Form Deformation
应用自由变形法的翼型几何外形参数化研究
16.
Topological optimization on the deformation mechanism of flexible trailing edge of certain pilot-less aircraft
某无人机柔性机翼后缘变形机构的拓扑优化
17.
The forces on an isolated tail are represented just like those on an isolated wing.
作用在单独尾翼上的力的表示方法正和单独机翼的情形一样。
18.
and the rms of both wing tips and apex reaches maximum value for elastic wing around the stall angle α=20°.
而在失速迎角α=20°附近,机翼顶点和翼梢变形的方差最大。