单词查询
airfoils
美['er.fɔɪl]，英['eə(r).fɔɪl]，
释义
「
」
na. 【航】机翼；翼形； 网络释义： 翼型；翼状物；机翼剖面；
例句
Sails are airfoils that work by using an airflow set up by the wind and the motion of the boat.
帆是翼型的工作使用气流所设立风和运动船。
Next, experimental investigations were completed in the wind tunnel on some modified airfoils with air jet.
其次进行了对某翼型被动喷气改型的风洞试验研究。
An assembly of rotating airfoils; horizontal rotors on a helicopter or compressor rotors of a jet engine.
旋转螺旋桨的集合；直升飞机上是水平旋转物，喷气式飞机上是压缩旋转物。
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。
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。
It has been applied to the design of compressor blades of some micro-engines, and fairly ideal airfoils are obtained.
通过在微小型发动机压气机叶片设计中的应用，得到了比较理想的叶片。
For steady incompressible flows, the effects of Reynolds number and thickness of airfoils on the aerodynamic characteristics are studied.
研究了在二维定常不可压流动状态下雷诺数和翼型厚度等参数对翼型气动特性的影响。
Its comprehensive coverage focuses on drag, turbulent flow, and vibration reduction in airfoils .
它的广泛报导集中在机翼阻力、湍流和振动减少。
All airfoils in this series will have four segments - the minimum number of segment.
所有翼型这四个环节将有一系列的最少数量部分。
The computational result shows that both the design of airfoils and the location of installation are reasonable.
计算结果表明，本算例中导流体的叶型设计和安装位置是合理的。
帆是翼型的工作使用气流所设立风和运动船。
Next, experimental investigations were completed in the wind tunnel on some modified airfoils with air jet.
其次进行了对某翼型被动喷气改型的风洞试验研究。
An assembly of rotating airfoils; horizontal rotors on a helicopter or compressor rotors of a jet engine.
旋转螺旋桨的集合；直升飞机上是水平旋转物，喷气式飞机上是压缩旋转物。
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。
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。
It has been applied to the design of compressor blades of some micro-engines, and fairly ideal airfoils are obtained.
通过在微小型发动机压气机叶片设计中的应用，得到了比较理想的叶片。
For steady incompressible flows, the effects of Reynolds number and thickness of airfoils on the aerodynamic characteristics are studied.
研究了在二维定常不可压流动状态下雷诺数和翼型厚度等参数对翼型气动特性的影响。
Its comprehensive coverage focuses on drag, turbulent flow, and vibration reduction in airfoils .
它的广泛报导集中在机翼阻力、湍流和振动减少。
All airfoils in this series will have four segments - the minimum number of segment.
所有翼型这四个环节将有一系列的最少数量部分。
The computational result shows that both the design of airfoils and the location of installation are reasonable.
计算结果表明，本算例中导流体的叶型设计和安装位置是合理的。