1.
Numerical Simulation of Active Stall Control on High-lift Airfoil
YLSG107高升力翼型主动流动控制的数值模拟
2.
"Airfoil: Shaped surface, such as an airplane wing, tail, or propeller Blade, that produces lift and drag when moved through the air."
翼型:在空气中运动时能产生升力和阻力的型面,如机翼、尾翼或螺旋桨桨叶。
3.
An Investigation for the Effects of Reduced Frequency on Aerofoil Dynamic Lift Characteristics
折算频率对翼型动态升力特性影响的初步研究
4.
An airfoil produces a lifting force that acts at right angles to the airstream and a dragging force that acts in the same direction as the airstream.
翼型产生升力的方向与气流成直角,阻力方向与气流方向相同。
5.
A Discussion on Lift and Moment Characteristics of Aerofoils in Incompressible Potential Flows
不可压缩位流中翼型升力及力矩特性的一点讨论
6.
Then the flight dynamics model of the ECR helicopter was constructed.
以此为基础,建立了电控旋翼直升机的飞行动力学模型。
7.
The configuration has two tractor propellers, full-span double slotted flaps deflected 45°, and a high tail.
实验模型有二两拉力螺旋桨，全翼展双缝襟翼偏转45°，并有高置的水平尾翼。
8.
fan-in-wing VTOL
翼内升力风扇式垂直起落飞机
9.
Dynamics analysis and modeling of helicopter rotor test-bed
直升机旋翼试验台动力学分析及建模
10.
The tail lift curve slope as determined from the panel model may require adjustment in order to apply the test results.
为了应用试验结果，根据翼段模型试验确定的平尾升力曲线斜率可能要作些修正。
11.
Study on Test,Data Acquisition and Processing Methods in Aerodynamics and Dynamics Experiments of Helicopter Rotor Model
直升机旋翼模型气动与动力学特性试验的测试与采集处理方法研究
12.
An upper canard, which is in the vicinity height of forward-swept main wing, could improve the maximum lift-to-drag ratio.
高于主机翼的鸭翼对最大升阻比的改善较多，但也不宜过高。
13.
"Airplane: Fixed-wing aircraft that is heavier than air, propelled by a screw propeller or a high-velocity jet, and supported by the dynamic reaction of the air against its wings."
飞机:用螺旋桨或高速喷射发动机推进和藉空气升力支持的各种重于空气的定翼航空器。
14.
The Application of Transonic Velocity Potential Equation with Higher Order Approximation for Computing the Pressure Distribution over the Blunt Leading-edge Airfoil
应用跨音速高级近似扰动速势方程计算钝前缘翼型的压力分布
15.
Much more increase of maximum lift-to-drag ratio can be obtained with a forward-swept main wing with a small sweepback angle leading edge.
主机翼前掠角较小时，鸭翼改善和提高升阻比的效果比较明显。
16.
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
17.
A variable control surface on the trailing edge of an aircraft wing, used primarily to increase lift or drag.
襟翼飞机后翼上最初用来增加上升力或拖力的可灵活控制的辅助翼
18.
Aerodynamics and Aerodynamic Heating Research for the Wing of Hypersonic Projectile;
高超声速弹箭尾翼（弹翼）的气动力与气动热研究