1.
rough air from stalled wing
失速机翼的扰动气流
2.
Canard wing increases lift coefficient with the penalty of the increase of drag coefficient.
低于主机翼的鸭翼将加强前掠翼布局的缓失速特性。
3.
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。
4.
Effects of Vortex Generators on Maximum Lift and Stall Angle of Attack over Wings
旋涡发生器对机翼最大升力和失速迎角的影响
5.
THE DESIGN OF AIRFOILS AND THE SIMULATION OF DYNAMIC STALL OF HORIZONTAL AXIS WIND TURBINES
水平轴风力机翼型设计与动态失速数值模拟
6.
Computations of Unsteady Aerodynamic Characteristic of Rotor Airfoil at Low Mach Numbers
旋翼翼型低Ma数动态失速特性计算
7.
NUMERICAL RESEARCH OF THE INFLUENCE OF AIRFOIL STALL AND REYNOLDS NUMBER CHANGE ON WIND TURBINE AERODYNAMIC PERFORMANCE
翼型失速及雷诺数变化对风力机气动性能影响的数值研究
8.
A TWO-DIMENSIONAL NUMERICAL STUDY ON STALL OF NACA4415 AIRFOIL
NACA4415翼型失速特性的二维数值研究
9.
Of all metal construction are wing structures of modern high-speed airplanes.
现代高速飞机的机翼全是金属结构的。
10.
A Static Aeroelastic Numerical Analytic Method of Transonic Flow About Wings
跨声速机翼静气动弹性数值分析方法
11.
Supersonic Nonlinear Fluutre Analysis of Dualistic Airfoil;
超音速流中二元机翼非线性颤振研究
12.
Investigation on Wing-Rotor Aerodynamic Interaction of the Compound Helicopter in Hover;
复合式高速直升机悬停状态旋翼/机翼气动干扰研究
13.
Experimental Investigation on Aerodynamic Interactions of Canard Rotor/Wing Aircraft in Hover and Low Speed Forward Flight
鸭式旋翼/机翼飞机悬停及小速度前飞气动干扰实验研究
14.
Aerodynamic Flutter and Limited Cycle of a 2-D Wing in the Hypersonic/Supersonic Flow Field
超声速/高超声速流中二元机翼的颤振与极限环
15.
If the wings are swept back, the plane will be faster.
如果机翼向后斜一点，飞机速度将会更快。
16.
a flap on the underside of the wing that is lowered to slow the plane for landing.
低的为飞机减速降落的在飞机外边的副翼。
17.
Rapid wing structure design and automated scheme adjustment for civil aircraft
民用飞机机翼结构快速设计及自动化调整
18.
Multi-disciplinary Optimization of Strut-braced Wing Transonic Transport
支撑机翼跨声速民机的多学科优化设计