英语释义

• a device that provides reactive force when in motion relative to the surrounding air; can lift or control a plane in flight

片语

aerofoil effect机翼效应

vane aerofoil叶片翼型

slotted aerofoil开缝机翼

airfoil机翼，翼型

isolated aerofoil孤立翼型

aerofoil blade叶片

aerofoil shape翼型形状

aerofoil lift气翼上升

aerofoil blading气翼翼系

aerofoil profile翼型

英汉例句

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

  旋转叶片的工作原理类似飞机的两翼，运用机翼的形状提供上升力。

• 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。

• although its aerofoil shape provides lift, a pilot needs to regulate the airflow over it in order to control the aircraft.

  虽然机翼的形状能够提供升力，飞机员还是需要调节通过其上的气流以达到控制飞机的目的。

• transformative problem of aerofoil impeller is put forward.

  提出了机翼型叶轮的改造问题。

• a new algorithm is presented for position regulating of aerofoil bracket on an automatic drilling and riveting machine.

  针对传统机翼壁板铆接过程中托架调平所存在的问题，提出一种基于有限曲面加工区域的三点调平算法。

• 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。

• it may obtain a special experiment aerofoil lift-drag force characteristic with this test.

  通过本实验，可以测得某一特定实验机翼的升力特性和阻力特性。

• the double-venturi wind-measuring device and aerofoil can meet the air quantity controlling requirements of the boiler under the reasonable collocation.

  在合理布置的情况下，双文丘利和机翼这两种测风装置都可以满足锅炉机组对风量测量的控制要求。

• pressurizing, continuous and transonic wind tunnel is the first one in our country , and it is the world's first class tremendous high- speed aerofoil wind.

  增压连续式跨音速风洞在我国尚属首例，是具有国际先进水平的大型高速翼型风洞。

• the most popular design methods of the axial fan are the single aerofoil method and the cascade method.

  其工程上的设计方法比较单一，普遍采用的方法是孤立叶型法和叶栅法。

• although its aerofoil shape provides lift, 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。

• 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。

• geometric characteristics for blade aerofoils during fan design, superposed aerofoils by analytic method, and the method to set up aerofoil circumference equation method are described.

  阐述了风机设计中叶片翼型的几何特性、用解析方法叠加翼型，以及建立翼型周线方程的方法。

• 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。

• 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 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。

• a good mechanics analysis approach was presented for reliability analysis and damage tolerance design of aerofoil structure.

  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。

• the design of the winglet on the wingtip of a plane is a multifactor design, it is relatively complicated in the design of an aerofoil due to the influence of no lesser parameters.

  飞机翼尖小翼设计是一个多因素设计，在机翼设计中比较复杂，影响参数较多。

• 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。

• 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。

• 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。

• 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。

• formulae for checking the strength of propeller with aerofoil and circular back sections are derived on the basis of analysis and empirical data.

  根据理论分析法，结合经验数据，分别推导出按拉应力或压应力的机翼型、弓型螺旋桨各强度校核公式与计算叶根处厚度公式。

• 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。