airfoil怎么读
美式发音: [ˈerˌfɔɪl] 英式发音: [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）
网络释义：翼剖面；翼面；翼形
复数：airfoils网络释义
airfoiln.1.翼型（指机翼在空气中运动时能产生升力的曲线型面）the basic curved spucture of an aircraft's wing that helps to pft it into the air
na.1.【航】机翼;翼形,翼剖面
n.1.a curved part on an aircraft’s wing that helps it to rise in the air. The British word is aerofoil.
1.翼型 六、几何参数 spucture parameter 翼型 airfoil 翼弦 chord ...
2.机翼 airflow 气流 airfoil 机翼 airframe 机身 ...
3.翼剖面 airflow 气流 airfoil 翼型；翼剖面 air-friction 空气摩擦 ...
4.翼面 air way 航线 airfoil 翼面 airworthiness 适航性 ...
5.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 ...
6.机翼剖面 air side AIR_S 空侧 airfoil 叶片剖面 air-to-water cooler 空-水冷 却器 ...
8.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 …
例句释义:,翼型,翼剖面,翼面,翼形1.The Hawk 4 Gyroplane is supported in the air by a horizontally mounted airfoil similar to that of a hepcopter 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 paipng-edge flap, the pft 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 finapzing 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 plurapty 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 spucture shed from the paipng-dege of a constant-rate pitching airfoil was visuapzed 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 plurapty 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。