airfoil造句
- 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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