1.
Numerical Investigation of Roll-angle Effect of the Vortex Flow on Double-delta Wing
静态滚转角对双三角翼涡流特性影响的数值研究
2.
Investigation on the Blade-Vortex Interaction Aerodynamic Noise of Helicopter Rotors;
直升机旋翼桨—涡干扰气动噪声的研究
3.
Effects of Leading-edge Vortex on Flutter Characteristics of High Sweep Angle Wing
大后掠翼前缘涡对其颤振特性的影响
4.
Turbulence in air or water caused by the motion or action of an oar, propeller, jet, or airfoil.
涡流由船桨、推进器、喷气机或机翼运动引起的空气或水的涡流
5.
Theoretical Model of the Large-Scale Eddy Structures in the Near Wake Region Behind an Airfoil
翼型近尾迹流中大尺度涡结构的理论模型
6.
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
7.
A numerical study of acoustic field radiated by uniform flow with a vortex past a profile
具有旋涡的翼型绕流辐射声场的数值研究
8.
Numerical Simulation of Unsteady Flows Past a Delta Wing by a 3-D Vortex Method;
三角翼周围非定常流动的三维涡方法数值模拟
9.
Visualization and measurement study of vortex flow over delta wing with dorsal fins
带背鳍平板三角翼分离涡流场的显示与测量
10.
The effects of trailing edge jets on the vortex breakdown location over a delta wing
三角翼后缘喷流对前缘涡破裂位置的影响
11.
Neural network control with model following for low aspect ratio flying wing based on vortex control
模型跟踪和涡流控制在飞翼布局飞机上的应用
12.
Research on rotor tip vortex model and the method for determining its parameter
旋翼桨尖涡模型及其参数确定方法研究
13.
New Type Support Design on Repair of South Wing Return Air Roadway in Guobei Coal Mine
涡北煤矿南翼回风大巷修复新型支护设计
14.
Experiment on flow control using Gurney-flaps for a low-pressure turbine cascade
基于Gurney襟翼的低压涡轮叶栅流动控制实验
15.
Lateral Inject Active Vortex Control Based on Low Aspect Ratio Flying Wing
小展弦比飞翼布局飞机横向涡流控制气动机理
16.
Frequency characteristics of breakdown vortices over delta wings with small amplitude oscillation at the high angle of attack
大迎角下小振幅振荡三角翼破裂涡的频率特性
17.
Large Eddy Simulation Study for Evolution of CoherentVortex Structure in Oscillatory Boundary Layer Flow over Flat-Plate or Winger-Type Wall
平板和翼型壁面上振荡流底边界层中拟序涡结构运动演化的大涡模拟研究
18.
This paper studied the wake improvement by stern fin and vortex generator numerically.
本文中利用数值计算讨论使用艉导流翼与涡流导流翼来改善艉迹流特性的可能性。