airfoil

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?

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2. An airfoil member comprising.
翼型会员包括。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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15. 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。

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16. 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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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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。

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