Numerical simulation on aerodynamic performance of an airfoil for wind turbine;
风力机叶片翼型气动特性数值模拟
Numerical simulation on airfoil stall separation suppression by plasma aerodynamic actuation;
等离子体气动激励抑制翼型失速分离的仿真研究
Numerical investigation of dynamic stall control using variable droop leading edge airfoil;
翼型动态失速的变下垂前缘控制数值模拟
Study of superlow speed aerofoil lift-drag force characteristic test;
超低速翼型升阻特性实验研究
Influence of boundary-layer separation of aerofoil under small angle of attack on the numerical simulation
小攻角下翼型边界层分离对数值模拟结果的影响研究
Numerical simulation on the aerodynamic performance of six kinds of aerofoil of wind turbine blade
6种风力机叶片翼型的气动性能数值模拟研究
Compared t o the other airfoils used in reversible fan design, the combined cascades are co nsidered to be super to th.
与现有的翼型相比 ,CN +Rymax 、αN +RCymax均有不同程度的提
Design research of high lift, mild stall airfoils (BUAA K1/BUAA K2) was conducted in order to investigate their design strategy, methods and technology for a long endurance aircraft.
为了探索适用于长航时飞行器的翼型设计思想、方法和技术 ,进行了新型高升力及失速特性缓和的BUAA K1 BUAA K2翼型的设计研究 。
An embedded H grid technique is employed for generating grids of isolated airfoils and cascades.
提出一种嵌入式 H型网格技术 ,用于生成孤立翼型和叶栅的计算网格。
Computation of Unsteady Pressure Distribution on a Profile in Transonic Flow;
二元翼型跨音速非定常压力计算
The influences of blade laying angle,solidity, blade shape,profile,blade relative thickness and impeller/hub ratio on the characters of impeller are calculated.
从搅拌桨的力与力矩平衡这两个基本方程出发，推导出轴流桨功率准数、流量准数与搅拌釜内能耗分配的理论计算式，并计算了桨叶的叶片安放角、盘面比、叶片形状、翼型、叶片的相对厚度、轮毂比对桨叶性能的影响。
The flow fields around a profile at a large attack angle with/without oscillating/steady excitation at the profile s leading edge have been numerical simulated.
本文数值模拟了施加振荡射流以及相应定常吸气条件下的翼型分离流动。
Experimental investigation on unsteady aerodynamics of rotor-blade airfoil;
旋翼翼型俯仰沉浮运动非定常气动特性实验研究
In the method, such an airfoil is termed a four-segment airfoil.
在方法,这种称为翼型四个部分机翼.
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
The Investigation of the Effect of Airfoil Modification on the Aerodynamic Performance of Supercritical Airfoil
翼型改型对超临界翼型气动性能影响的研究
kormon trefftz profile
卡门 特雷夫茨翼型
Kutta-Joukowski airfoil
库塔-儒科夫斯基翼型
Aerodynamic Characteristic Computations on Iced Airfoils、Multi-Element Airfoil and Rudder;
结冰后翼型、多段翼型及舵面的气动特性计算
Airfoil design of a micro-flapping wing based on CFD
基于CFD方法对微型扑翼翼型设计的研究
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.
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.
Cross Wing of Diamond Wing Profile and Isosceles Trapezoid Wing Surface for Course Correction Fuze
弹道修正引信菱形翼型等腰梯形十字减旋翼
Numerical Simulation of Usteady Flows over Gliding Flap of Multi-element Airfoils
多段翼型襟翼滑动非定常粘性流数值模拟
A New Mesh-Free Difference Method Applied to Compressible Flow Past a Two-Dimensional Airfoil
二维可压翼型绕流的新型无网格解法
In this regard, several airfoil templates are given based on existing designs, eg, the SD7037 airfoil and others.
在这方面,有几个版本,基于现有翼型设计,例如,sd7037翼型等.
The effects of wind-tunnel model design on flowfield and aerodynamic behavior for large aspect-ratio wings
大展弦比机翼模型设计对翼型流场气动特性的影响
Effect of Aerofoil Camber on Airfoil Aerodynamic Performance
风力机的翼型弯度对风力机翼型气动性能的影响
"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。
In the design page, submit the form to design the first airfoil.
在设计页,递交表格设计第一翼型.
A variant of the swept-back wing is the delta wing.
后掠翼的变型是三角翼。