aerofoil
美 [ˈerəˌfɔɪl] 
英 [ˈeərəˌfɔɪl]
- n.翼型（指机翼在空气中运动时能产生升力的型面）
- 网络翼面；风板；翼剖面
词形变化
复数：aerofoils
英汉双解
1. | 翼型（指机翼在空气中运动时能产生升力的型面）the basic curved structure of an aircraft's wing that helps to lift it into the air |
英汉解释
英英解释
例句
The aerofoil of a wing creates more lift than drag, but exactly how much depends on its design and the speed of the air passing over it.
飞机上的机翼制造升力超过阻力，但具体取决于机翼的设计和当时经过的空气流动速率。
The aerodynamic characteristic of moving aerofoil on the surface of inclined plate and of ordinary plane varies much.
在斜板表面和常规平板表面上运动的机翼的气动力性能有所不同。
The rotor blades work like the wings of an aeroplane, with an aerofoil shape providing lift.
螺旋桨起的作用如同飞机的机翼，机翼的形状提供升力。
The blades have an aerofoil shape and provide lift when passing through air, like the wings of an aeroplane.
这些叶片拥有机翼的剖面形状，它们就像普通飞机的机翼那样，通过划过空气来产生升力。
The deck is an orthotropic steel box girder of aerofoil shape with cantilevered cycle tracks and footway supported from the box.
桥面板采用翼型正交异性钢箱梁结构，由钢箱支撑起悬臂式自行车专用道和人行道。
The effects of flapping frequency, wind velocity, angle of attack, plane shape of wing and cambered aerofoil are investigated.
试验中进行了扑动频率、风速、迎角、机翼平面形状、翼型弯度对机翼气动特性影响的研究。
Its aerofoil shape provides lift, but a pilot needs to regulate the airflow over it in order to control the aircraft.
虽然机翼的外形提供了飞机的升力，但驾驶员还需要通过调节掠过机翼的气流来操纵飞机。
Reducing the maximum thickness of aerofoil can improve the stage profile efficiency.
减小叶栅最大相对厚度可以提高叶型效率。
By adopting the particle swarm algorithm the optimal solution on the layout of composite material aerofoil structure was carried out.
采用粒子群算法对复合材料机翼结构进行布局优化求解。
nf - 6 wind tunnel is a pressurizing , continuous , high - speed and return - flow aerofoil wind tunnel.
6风洞是一座由轴流式压缩机驱动的增压、连续、高速回流式翼型风洞。
The serpentine aerofoil shape is designed to face into what little wind there is, generating a small amount of lift.
蛇形蜷曲的机翼设计用来面对空中的较小风力去产生一个较小的升力。
Loss of head is minimized by the balanced disc and its aerofoil design.
通过平衡阀瓣及其“翼型”结构，将水头损失（或位差损失）降到最小程度。
Optimal design on aerofoil parameter of impeller is made based on the second YQH-100 oil-gas pump.
基于第二代YQH-100油气混输泵叶轮的基本参数，对叶轮的翼型参数进行了优化设计。
A numerical study of aerodynamic characteristics of modified aerofoil with a blunt trailing edge
翼型进行钝尾缘修改后气动性能的数值研究
Experimental Investigation of Aerodynamic Characteristics of the Air-cushion Anti-erosion Fan Aerofoil
风机气垫防磨叶片表面压力实验研究
An investigation on boundary flow of aerofoil controlled by electromagnetic force
电磁力控制翼型体边界层流动的研究
Experimental Study of Cavitation Damage Behaviors of NiAl alloyed Aerofoil
NiAl合金翼型空蚀破坏行为的试验研究
CFD Analysis of Aerodynamic Characteristics for the Ducted Tail Rotor and Its Aerofoil
涵道尾桨气动特性及翼型CFD分析
Numerical Simulation and Performance Prediction of Reversible Pump with Symmetric Aerofoil
对称翼型转轮双向泵装置紊流数值模拟与性能预测
Test Analysis on Main Characteristic Parameters of Multi-aerofoil Centrifugal Fan Impeller
多翼离心通风机叶轮主要特征参数的试验分析
Numerical simulation for the extruding of compressed aerofoil parts and the flaw prediction
扁翼类零件挤压成形数值模拟及缺陷预测
On the hydrodynamic forces of submersible with aerofoil section in forward and backward motions
扁平潜器微速与倒航水动力试验研究
A Study on Geometric Methods for Designing Supersonic Aerofoil of Axial Flow Compressor
轴流压气机超音叶片叶型几何设计方法的研究
Kinetic System Design for Aerofoil Integral Fuel Tank Cleaning Equipment
机翼整体油箱清洗设备运动系统的设计
Experiments of the flow field structure control around an aerofoil based on electromagnetic force
用电磁体积力的翼型绕流控制实验研究
Fatigue Failure Analysis of Aerofoil Girder Leading to Air Disaster
导致空难的机翼大梁的疲劳失效分析
Effect of Axial Flow Pump Performance of Anti-cavitation Through Choice of Aerofoil
翼型的选择对轴流泵抗汽蚀性能的影响
Optimization Technique in Inverse Design of Fan Blade Aerofoil
风机叶片的剖面翼型反设计优化技术
Finite Element Analysis of Aerofoil Fatigue Failure
飞机机翼疲劳断裂过程的有限元分析
Optimization design of aerofoil structure based on neural network and hybridization algorithm
基于神经网络与杂交算法的机翼结构优化设计
The design of new intelligent flowmeter based on Aerofoil principle
基于机翼原理新型智能应变流量计的设计
Parameterized aerofoil structure design based on surface
基于曲面的飞机机翼结构参数化设计
