1.
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
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.
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
5.
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。
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.
fan-in-wing VTOL
翼内升力风扇式垂直起落飞机
8.
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
9.
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。
10.
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
11.
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
12.
DESIGN AND RESEARCH FOR A NEW TYPE BUOYANCY-LIFTING ROW FLYING-WINGS
一种新型浮升一体化排式飞翼的设计与研究
13.
Support Vector Machine Model for Landing Process of Helicopter with Rotator Self-rotating
直升机旋翼自转着陆过程的支持向量机模型
14.
a movable airfoil that is part of an aircraft wing; used to increase lift or drag.
机翼的可活动的一部分；用来增加升拉力量。
15.
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
16.
Unsteady Aerodynamics Investigation for the Isolated Rotor in Large Amplitude Maneuvering Flight;
直升机大机动飞行中旋翼非定常空气动力研究
17.
Hinge Moment Acquisition and Transmission Research in the Helicopters Airscrew Dynamic-balancing Test Platform;
直升机旋翼动平衡台铰链力矩测量与传输研究
18.
Dynamic model of elastic impact of helicopter rotor blades
直升机旋翼桨叶的弹性碰撞动力学建模