airfoil
美 [ˈerˌfɔɪl]英 [ˈeə(r)ˌfɔɪl]
- n.翼型（指机翼在空气中运动时能产生升力的曲线型面）
- 网络翼剖面；翼面；翼形
复数：airfoils
airfoilairfoil
翼型
风机英语术语_百度文库 ... 六、几何参数 structure parameter 翼型 airfoil 翼弦 chord ...
机翼
英语新词汇与常用词汇的翻译(A) ... airflow 气流 airfoil 机翼 airframe 机身 ...
翼剖面
阀门英语单词（杨玉飞整理） ... airflow 气流 airfoil 翼型；翼剖面 air-friction 空气摩擦 ...
翼面
民航专业常用词汇指南(ME)[1]_百度文库 ... air way 航线 airfoil 翼面 airworthiness 适航性 ...
翼形
... airflow;supercritical 超临界气流 airfoil 翼形;翼切面 airfoil aerodynamic center 翼形气动力中心 ...
机翼剖面
名词解释: 飞机机翼剖面(airfoil)的弦线和自由流(freestream)的夹角称为攻角，如图所示。攻角愈大，则上翼剖面的气流速度愈 …
叶片剖面
热能工程专业英语_百度文库 ... air side AIR_S 空侧 airfoil 叶片剖面 air-to-water cooler 空-水冷 却器 ...
翼型进气口
...当前窗处于全开启状态下，气流通过前 窗开口以及前方翼型进气口(Airfoil)流入 2. 当前窗高度降至50%开启，气流通过前 窗 …
1
The Hawk 4 Gyroplane is supported in the air by a horizontally mounted airfoil similar to that of a helicopter but unpowered .
鹰4旋翼机利用类似直升机的旋翼提供升力，但机顶的水平旋翼无需动力推动。
2
and for that of a trailing-edge flap, the lift of the airfoil or separating position at the key airfoil element is used.
对后缘襟翼则分别以翼型升力值和分离点位置作为间接目标函数，进行优化计算。
3
The afterbody form finalizing sheet is in an arc shape, the tail part raises upwards to assist the airfoil to be the arc.
机尾定型片呈弧形，其尾部上翘，辅助机翼成弧形。
4
said airfoil means includes a plurality of airfoil form retaining means for supporting and defining the chord length of said airfoil means.
说翼型的手段，包括多元化的翼型的形式保留的手段，支持和界定弦长的说，翼型的手段。
5
This thesis investigated the effect of the airfoil modification on the aerodynamic performance of a certain supercritical airfoil.
鉴于此，本文选取某超临界翼型，探讨改型对超临界翼型气动性能的影响。
6
The vortex structure shed from the trailing-dege of a constant-rate pitching airfoil was visualized using hydrogen bubble technique.
在尾缘处置氢气泡铂丝，观察了上仰翼型自尾缘流入尾迹的涡层。
7
a plurality of airfoil form retaining members for defining the chord length of said second airfoil means.
多元化的翼型的形式保留成员的界定弦长的说，第二翼型的手段。
8
The results showed that the aerodynamic performance of the airfoil could be improved when properly added its thickness.
结果表明，适当增加翼型厚度可以提高翼型的气动性能。
9
An airfoil adapted to be supported on an aircraft fuselage comprising.
翼型适应予以支持对飞机机身组成。
10
The wake survey cannot be used to measure the drag of stalled airfoil or of airfoils with flaps down.
尾流测量不能用来测量失连状态下的冀型或襟翼偏转后的翼型阻力。
11
Airfoil trailing-edge vortex separation occurs, resulting in movement of the flow field near the airfoil stall.
翼型后缘出现的分离涡，导致翼型附近流场的流动失速。
12
Optical lift is different from the aerodynamic lift created by an airfoil.
光学提拉力与机翼翼面产生的空气动力不同。
13
Aimed at above problems, the thesis conducted research on wind turbine dedicated airfoil and its design and analysis methodology.
针对以上的问题，本论文主要针对风机新翼型及其气动性能进行研究。
14
Numerical results of a design example show that the airfoil design method is effective and robust.
结果表明，所采用的翼型设计方法是正确、有效的。
15
Fairly ideal airfoils were obtained. This method of airfoil design has been validated to be operational and applicable by CFD simulation.
通过CFD流场检验验证了这种叶片造型方法的可操作性和适用性。
16
Its airfoil is installing a gun above backward incline, the airfoil end is still having two guided missiles.
它的机翼向后倾斜，上面装着枪，机翼结尾还有两枚导弹。
17
Surface pressure distribution can be used to describe the airfoil boundary layer flow well.
表面压力分布曲线可以较好的描述翼型边界层流动。
18
In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology(RSM).
基于响应面方法进行了跨声速翼型的气动优化设计。
19
Applications include coupling boots, fuselage and hatch seals, aerodynamic sealing of airfoil surfaces and jet engine compressor stages.
应用范围包括耦合，机身和舱口密封，机翼面和喷气发动机压气机级的气动密封。
20
Provide an airfoil at the sill of the sash opening. It shall be mounted to provide a 1 inch slot above the hood interior counter top.
开口拉门处有一个翼面，安装时应在内部台面上留有1英寸的狭缝。
21
The airfoil-shaped measuring flume water head loss isn't higher, and the water head losing has 14% of the total head of water.
机翼形量水槽的水头损失不大，水头损失约占上游总水头的14%左右。
22
The ice accretion geometric characteristics have complex effects on airfoil aerodynamic coefficients.
积冰几何形状对翼型气动系数的影响是复杂的。
23
The leading edge portion includes a plurality of staggered holes for causing fluid to flow over a surface of the airfoil portion.
该前缘部包括多个错开的孔以便使流体在该翼面部的表面上流动。
24
The aerodynamic characteristics of airfoil are significantly influenced by non-equilibrium condensation of moist air.
湿空气非平衡凝结会对机翼的气动特性造成显著影响。
25
By numerical simulation method, the comparisons of aerodynamic performance between airfoil and plate blade axial fans were made.
采用数值模拟方法对机翼型及板型叶片的轴流风机的气动性能进行了比较。
26
It is further displayed that the testing technique of flexible adaptive walled wind tunnel could apply to future transonic airfoil testing.
实验结果展示了自适应壁风洞实验技术用于翼型跨音速实验的前景。
27
a second leading edge member defining the cross-sectional configuration of said second airfoil means.
第二个领先的会员界定的横截面的配置说，第二翼型的手段。
28
Numerical results show that the method provides an effective tool for refining and designing a transonic airfoil.
算例结果表明，本方法提供了一种跨音速翼型改型设计及新翼型设计的有效工具。
29
Airfoil buffeting boundary is an important aerodynamics targets which second only to the lift-drag ratio.
翼型抖振边界是仅次于升阻比的一项重要气动指标。
30
A turbine engine component has an airfoil portion with a leading edge portion.
一种涡轮发动机构件具有一个翼面部，其上有一前缘部。