aerofoil

aerofoil

美 [?er??f??l] 　英 [?e?r??f??l]

• n.翼型（指機翼在空氣中運動時能產生升力的型面）
• 網絡翼面；風板；翼剖面

詞形變化

復數：aerofoils  

英漢雙解

英漢解釋

n.	1. 【航】機翼;翼型;翼剖面

英英解釋

n.	1. an airfoil

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.

飛機上的機翼制造升力超過阻力，但具體取決于機翼的設計和當時經過的空氣流動速率。

The aerodynamic characteristic of moving aerofoil on the surface of inclined plate and of ordinary plane varies much.

在斜板表面和常規平板表面上運動的機翼的氣動力性能有所不同。

The rotor blades work like the wings of an aeroplane, with an aerofoil shape providing lift.

螺旋槳起的作用如同飛機的機翼，機翼的形狀提供升力。

The blades have an aerofoil shape and provide lift when passing through air, like the wings of an aeroplane.

這些葉片擁有機翼的剖面形狀，它們就像普通飛機的機翼那樣，通過劃過空氣來產生升力。

The deck is an orthotropic steel box girder of aerofoil shape with cantilevered cycle tracks and footway supported from the box.

橋面板采用翼型正交異性鋼箱梁結構，由鋼箱支撐起懸臂式自行車專用道和人行道。

The effects of flapping frequency, wind velocity, angle of attack, plane shape of wing and cambered aerofoil are investigated.

試驗中進行了撲動頻率、風速、迎角、機翼平面形狀、翼型彎度對機翼氣動特性影響的研究。

Its aerofoil shape provides lift, but a pilot needs to regulate the airflow over it in order to control the aircraft.

雖然機翼的外形提供了飛機的升力，但駕駛員還需要通過調節掠過機翼的氣流來操縱飛機。

Reducing the maximum thickness of aerofoil can improve the stage profile efficiency.

減小葉柵最大相對厚度可以提高葉型效率。

By adopting the particle swarm algorithm the optimal solution on the layout of composite material aerofoil structure was carried out.

采用粒子群算法對復合材料機翼結構進行布局優化求解。

nf - 6 wind tunnel is a pressurizing , continuous , high - speed and return - flow aerofoil wind tunnel.

6風洞是一座由軸流式壓縮機驅動的增壓、連續、高速回流式翼型風洞。

The serpentine aerofoil shape is designed to face into what little wind there is, generating a small amount of lift.

蛇形蜷曲的機翼設計用來面對空中的較小風力去產生一個較小的升力。

Loss of head is minimized by the balanced disc and its aerofoil design.

通過平衡閥瓣及其“翼型”結構，將水頭損失（或位差損失）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油氣混輸泵葉輪的基本參數，對葉輪的翼型參數進行了優化設計。

A numerical study of aerodynamic characteristics of modified aerofoil with a blunt trailing edge

翼型進行鈍尾緣修改后氣動性能的數值研究

Experimental Investigation of Aerodynamic Characteristics of the Air-cushion Anti-erosion Fan Aerofoil

風機氣墊防磨葉片表面壓力實驗研究

An investigation on boundary flow of aerofoil controlled by electromagnetic force

電磁力控制翼型體邊界層流動的研究

Experimental Study of Cavitation Damage Behaviors of NiAl alloyed Aerofoil

NiAl合金翼型空蝕破壞行為的試驗研究

CFD Analysis of Aerodynamic Characteristics for the Ducted Tail Rotor and Its Aerofoil

涵道尾槳氣動特性及翼型CFD分析

Numerical Simulation and Performance Prediction of Reversible Pump with Symmetric Aerofoil

對稱翼型轉輪雙向泵裝置紊流數值模擬與性能預測

Test Analysis on Main Characteristic Parameters of Multi-aerofoil Centrifugal Fan Impeller

多翼離心通風機葉輪主要特征參數的試驗分析

Numerical simulation for the extruding of compressed aerofoil parts and the flaw prediction

扁翼類零件擠壓成形數值模擬及缺陷預測

On the hydrodynamic forces of submersible with aerofoil section in forward and backward motions

扁平潛器微速與倒航水動力試驗研究

A Study on Geometric Methods for Designing Supersonic Aerofoil of Axial Flow Compressor

軸流壓氣機超音葉片葉型幾何設計方法的研究

Kinetic System Design for Aerofoil Integral Fuel Tank Cleaning Equipment

機翼整體油箱清洗設備運動系統的設計

Experiments of the flow field structure control around an aerofoil based on electromagnetic force

用電磁體積力的翼型繞流控制實驗研究

Fatigue Failure Analysis of Aerofoil Girder Leading to Air Disaster

導致空難的機翼大梁的疲勞失效分析

Effect of Axial Flow Pump Performance of Anti-cavitation Through Choice of Aerofoil

翼型的選擇對軸流泵抗汽蝕性能的影響

Optimization Technique in Inverse Design of Fan Blade Aerofoil

風機葉片的剖面翼型反設計優化技術

Finite Element Analysis of Aerofoil Fatigue Failure

飛機機翼疲勞斷裂過程的有限元分析

Optimization design of aerofoil structure based on neural network and hybridization algorithm

基于神經網絡與雜交算法的機翼結構優化設計

The design of new intelligent flowmeter based on Aerofoil principle

基于機翼原理新型智能應變流量計的設計

Parameterized aerofoil structure design based on surface

基于曲面的飛機機翼結構參數化設計