Experimental research on airfoil-shaped flow flume;
机翼形量水槽的试验研究
Experiment on Airfoil-shaped Measuring Flume in Trapezoidal Canal
梯形渠道机翼形量水槽试验
In order to simulate the bird flying,we design a three-dimensioal morphing aircraft wing.
为了模仿鸟类的飞行,利用杆索柔性机构的杆变形特性和柔性索为驱动,采用结构优化方法设计三维展向变形机翼,使其在各种飞行状态下都能保持最优气动性能。
Analysis of Stretching Deformation of the Spiral Wing Drive Mechanism Many Flexible Body Simulation
伸缩机翼变形机构多柔性体动力学仿真分析
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
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
camber changing flap
改变机翼弯度的襟翼
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
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。
Topology Optimization for Shape Morphing Compliant Trailing Edge Using SIMP and GA
基于SIMP和GA变形柔性机翼后缘的拓扑优化
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
Another innovation will be the use of variable geometry - the wings will have two positions.
另一项创新是使用变几何形状布局，即机翼可有两个位置。
On Conformal Transformation Constituted by the Function of Wing’s Section, It’s Inverse Function and Their Application;
机翼剖面函数及其反函数构成的保形变换与应用
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.
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.
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
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
The mathematical transformation is fixed and the airfoil is moved to generate different airfoil geometries.
数学变换是固定机翼的翼型几何移到产生不同.
delta wing (hang gliders)
三角形机翼（悬挂式滑翔机）
Analysis of Thermal-elastic Deformation for Solar Array Substrate with CFRP/Aluminum Honeycomb Sandwich
碳纤维/铝蜂窝太阳翼基板热变形分析
Study on control of morphing wings based on microsystems arrays
基于微系统阵列的变形翼的控制研究
