airfoil
n. 机翼；螺旋桨
n.
机翼，螺旋桨；翼面；
英英释义
airfoil[ 'εəfɔil ]
n.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：aerofoilcontrol surfacesurface
权威例句
Airfoil Theory for Non-Uniform MotionAirfoil and Bridge deck flutter derivatives
Airfoil and bridges deck flutter derivatives
Unsteady Euler airfoil solutions using unstructured dynamic meshes
Large Eddy Simulation of Flow Around an Airfoil Near Stall
Vortical patterns in the wake of an oscillating airfoil
Computation of oscillating airfoil flows with one- and two-equation turbulence models
Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
Numerical study of the turbulent flow past an airfoil with trailing edge separation
Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators
airfoil (n.)
1922, U.S. form of aerofoil.
1. How does the brake act on the paraglider airfoil?
刹车是如何作用于滑翔伞的机翼的？
youdao
2. An airfoil member comprising.
翼型会员包括。
youdao
3. The airfoil member according to claim 1, further comprising.
翼型会员根据权利要求1，进一步包括。
youdao
4. In the design page, submit the form to design the first airfoil.
在设计页，递交表格设计第一翼型。
youdao
5. In the method, such an airfoil is termed a four-segment airfoil.
在方法，这种称为翼型四个部分机翼。
youdao
6. 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。
youdao
7. An airfoil as recited in claim 17, wherein said airfoil means includes.
翼型作为背诵，在索赔17，其中，表示翼型的手段包括。
youdao
8. 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。
youdao
9. The given airfoil is then analyzed to determine, say, its velocity distribution.
由于机翼的分析，以确定那是说，它的速度分布。
youdao
10. So for Mid reflection airfoil, the wing could fly normally with only A and B anchor.
所以对于中反射翼型来说，只要A，B 两组绳就能正常飞行。
youdao
11. And it loses more and more as we follow it along the path close to the solid airfoil.
和它失去了越来越多的我们按照它沿路径接近了坚实的翼型。
youdao
12. The airfoil member according to claim 1, configured as a wing of a non-rotor aircraft.
翼型会员根据权利要求1，配置为一翼，非翼飞机。
youdao
13. The airfoil member according to claim 1, configured as a rotor blade for a helicopter.
翼型会员根据权利要求1 ，配置为转子叶片为直升机。
youdao
14. The various design parameters are introduced before moving on to a six-segment airfoil.
各设计参数介绍转学至六部分机翼。
youdao
15. You can specify wing attributes including camber and centerline sheeting of an airfoil.
你能够标示翅膀归结于包括中凸形和机翼的中心线护墙板。
youdao
16. Researching the adaptation of airfoil lays the foundation for designing adaptive wings.
二维翼型自适应的研究是设计自适应机翼的基础。
youdao
17. The high speed airfoil type wind turbine has the highest efficiency in high wind speeds.
高速机翼型风轮机在高风速下达到最高的使用效率。
youdao
18. Provide the experimental research scheme to measure and diagnose boundary layer of airfoil.
根据附面层流动特性，提出了附面层综合测量和诊断实验研究方案。
youdao
19. The effectiveness of using plasma actuation to suppress airfoil stall separation is verified.
验证了等离子体激励抑制翼型失速分离的有效性。
youdao
20. The system of claim 1, further comprising an aircraft, the airfoil being coupled to the aircraft.
该系统的索赔1，进一步组成的飞机，加上正在翼型飞机。
youdao
21. The system of claim 11, further comprising an aircraft, the airfoil being coupled to the aircraft.
该系统的索赔11，进一步组成的飞机，加上正在翼型飞机。
youdao
22. The system of claim 16, further comprising an aircraft, the airfoil being coupled to the aircraft.
该系统的索赔16，进一步组成的飞机，加上正在翼型飞机。
youdao
23. There will be some compromising in the selection of the airfoil - but the airfoil is only one parameter.
会有一些妥协，在遴选的翼型-但翼型只有一个参数。
youdao
24. Direct methods are based on the design-by-analysis approach in which the airfoil shape is specified first.
直接的方法是基于设计逐案分析的方法是机翼形状指定第一。
youdao
25. The STOL ch 801 USES a special airfoil design to achieve very high lift, low stall speeds, and high strength.
甲烷的短距起落801使用一个特殊的翼型设计，达到非常高扬程，低失速速度，强度高。
youdao
26. The Web version of the code allows for the prescription of the inviscid velocity distribution about the airfoil.
网上版的代码允许处方粘速度分布的翼型。
youdao
27. To put the method in some perspective, it helpful to briefly outline the two general approaches to airfoil design.
把一些观点方法，它有助于扼要介绍两个一般方式翼型设计。
youdao
28. For pure pitching motion, the results show that average drag coefficient decreases as airfoil thickness is reduced.
在低雷诺数条件下，对于纯俯仰运动，随着翼型厚度的减小，平均阻力系数也变小。
youdao
29. For pure pitching motion, the results show that average drag coefficient decreases as airfoil thickness is reduced.
在低雷诺数条件下，对于纯俯仰运动，随着翼型厚度的减小，平均阻力系数也变小。
youdao
30. airfoil profile
翼型
-- 来源 -- 英汉 - 短句参考
31. aerofoil; airfoil
翼面;空气动力面
-- 来源 -- 英汉 - 翻译样例 - 工程
32. airfoil cascade
导向叶片系
-- 来源 -- 英汉 - 翻译参考[网络]
33. laminar flow airfoil
层流翼型
-- 来源 -- 英汉 - 翻译参考[网络]
34. stalled airfoil
失速机翼
-- 来源 -- 英汉 - 翻译参考[网络]
35. airfoil element
机翼型元件
-- 来源 -- 英汉 - 翻译参考[网络]
36. airfoil section
翼剖面;翼型
-- 来源 -- 英汉 - 翻译参考[网络]
37. Kutta-Joukowski airfoil
库塔-儒科夫斯基翼型
-- 来源 -- 英汉 - 翻译参考[网络]
38. airfoil characteristic
翼型特性
-- 来源 -- 英汉 - 翻译参考[网络]
39. airfoil-section funnel
翼型截面烟囱
-- 来源 -- 英汉 - 翻译参考[网络]
airfoil
