aerofoil
['ɛərəfɔil]
n.翼型,翼剖面,机翼
n.
【空】机翼; 翼剖面
aerofoil
aerofoil['εərəfɔil]n.1.■[主英国英语] = airfoil
aerofoilaerofoil[ˈɛərəfɔil]n.1.■机翼; 翼型; 翼剖面2.■导风罩[板]
noun
- (Brit.)a structure with curved surfaces designed to give the most favourable ratio of lift to drag in flight, used as the basic form of the wings, fins, and tailplanes of most aircraft
(英)翼型,翼面
aerofoil
名词 aerofoil:
a device that provides reactive force when in motion relative to the surrounding air; can lift or control a plane in flight
同义词:airfoil, control surface, surface
aerofoil
■1 new aerofoil design :the paddle ,which is manufactured according to the structure and process of propeller aircraft.the generator can use in 15-20 years.
1新型翼型设计:浆叶按照飞机螺旋桨的结构和工艺制造,坚固耐用,电机设计使用寿命15-20年.
■The name Aeroform is derived from the term aerofoil, which is a structure having a shape that provides stability, or directional control in a flying object.
Aeroform的名字来源于术语aerofoil(机翼),该结构外形具有极佳的稳定性(或飞行物定向控制力)。
■Jameson/TVD Schemes Applied to Simulating the Flow around Rotor Aerofoil
Jameson/TVD格式应用旋翼翼型绕流分析
■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
■Keywords TC6 titanium alloy;Aerofoil blade;Grain size;Numerical simulation;
TC6合金;叶片;晶粒尺寸;数值模拟;
■tripe cambered aerofoil
[机] 三曲翼面
■reflex curvature aerofoil
[机] 上翘翼面
■top aerofoil
[机] 上翼面
■lower aerofoil
[机] 下翼面
■bottom aerofoil
[机] 下部翼剖面
■tapered aerofoil
[机] 不等弦翼面
■front slot aerofoil
[机] 前缝翼面
■single cambered aerofoil
[机] 单曲翼面
■double courved aerofoil
[机] 双曲翼剖面
■double cambered aerofoil
[机] 双曲翼面
■symmetrical aerofoil
[机] 对称翼面
■laminar flow aerofoil
[机] 层流翼面
■aerofoil of infinite
[机] 无限展翼
■aerofoil of finite span
[机] 有限展翼
■non-tapered aerofoil
[机] 等弦翼面
■supersonic aerofoil
[机] 超声速翼面
■high speed aerofoil
[机] 高速翼面
■triple cambered aerofoil
三曲翼面
■upper aerofoil
上翼面
■A good mechanics analysis approach was presented for reliability analysis and damage tolerance design of aerofoil ...
为机翼结构的可靠性分析和损伤容限设计提供了比较有价值的力学分析手段。
■Main rotor is the key part of helicopter modeling,the associated modeling methods of aerofoil aerodynamic loads,rotor inflow dynamics and blade flap motion are discussed in detail.
主旋翼是直升机建模的关键,详细讨论了与其相关的翼型气动力模型、诱导速度模型和挥舞运动模型的建模方法。
■The author modifies spanwise shape and makes the analog function of the aerofoil curve by use of the computer.
利用计算机来辅助叶片叶展形状的修正和构造翼型曲线的模拟函数。
■Keywords double speed motor;front leaves adjusted;aerofoil leaves;intelligent actiyator;
双速电机;可调前导叶;机翼型叶片;智能调速;
■backward aerofoil blade
反向流线形叶片
■variable sweep aerofoil
可变后掠翼
■This paper describes the investigation of boundary layer separation control for supercritical aerofoil using micro vortex generator in the low speed wind tunnel.
在低速风洞中研究了微型涡流发生器对超临界翼型边界层分离的控制。
■Aerofoil Optimization of Fluid Machinery Based on CAD/CFD System
基于CAD/CFD分析系统的流体机械翼型优化
■Research of Test and Control System Based on VI for Bracket of Aerofoil Automatic Rivet Machine
基于虚拟仪器的机翼自动钻铆机托架测控系统的研究
■Single aerofoil method
孤立翼型法
■The numerical results for the lift and the drag hysteresis associated with a NACA0012 aerofoil oscillating in pitch are good in comparison with available experimental data.
对俯仰谐振的NACA0012翼型所计算得的升力和阻力的滞后现象,与实验结果相一致
■symmetric aerofoil
对称翼型
■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
■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
■laminar aerofoil section
层另型
■The incidence angle and deviation angle can be given freely in the process of aerofoil design, the satisfied aerofoil of fan blade is obtained through velocity distribution optimization.
并且在设计中可以自由给定攻角、落后角,通过速度分布的优化得到符合工程应用要求的风机叶片的翼型。
■Three kinds of fan blade aerofoil have been designed according to the velocity distribution optimization criterion.
并依据探索出的速度分布优化准则,设计出了三种风机叶片的翼型。
■Some exemples to apply the aerofoil computed from these formula to the fan design are listed. ?
并列举了利用其公式算出的翼型在风机设计上的应用实例。
■3.With use of this structure model, we can simulate the real performance of aerofoil very well.
应用该结构模型可以很好的模拟机翼结构的实际情况。
■slotted aerofoil
开缝机翼
■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
■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
■Keywords compressed aerofoil part;cold extrusion;numerical simulation;
扁翼零件;冷挤压;数值模拟;
■An Investigation for the Effects of Reduced Frequency on Aerofoil Dynamic Lift Characteristics
折算频率对翼型动态升力特性影响的初步研究
■Ac- cording to these methods, we have calculated two aerofoil drag coefficients under different Reynolds numbers and Mach numbers.
按照上述方法计算了在不同雷诺数和不同马赫数下两个翼型剖面的摩阻系数。
■Provided with high performing adjustable pitch aerofoil impellers in PAG, aluminum, steel and stainless steel.
提供上流执行的可调整的沥青机翼叶轮在PAG,铝,钢和不锈钢。