• How does the brake act on the paraglider airfoil?

    刹车如何作用于滑翔伞机翼的?

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  • An airfoil member comprising.

    会员包括

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  • Airfoil design technology and criterion are investigated.

    进行了叶型设计技术准则研究

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  • The airfoil member according to claim 1, further comprising.

    会员根据权利要求1进一步包括

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  • In the design page, submit the form to design the first airfoil.

    设计递交表格设计第一翼型

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  • In the method, such an airfoil is termed a four-segment airfoil.

    方法这种称为型四部分机翼

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  • An airfoil adapted to be supported on an aircraft fuselage comprising.

    适应予以支持飞机机身组成。

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  • An airfoil as recited in claim 17, wherein said airfoil means includes.

    作为背诵索赔17其中表示翼型的手段包括

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  • Optical lift is different from the aerodynamic lift created by an airfoil.

    光学拉力与机翼翼面产生的空气动力不同

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  • The given airfoil is then analyzed to determine, say, its velocity distribution.

    由于机翼的分析确定速度分布。

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  • So for Mid reflection airfoil, the wing could fly normally with only A and B anchor.

    所以对于反射翼型来说,只要AB 两组正常飞行

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  • And it loses more and more as we follow it along the path close to the solid airfoil.

    失去了越来越多的我们按照沿路径接近坚实的翼型。

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  • The airfoil member according to claim 1, configured as a wing of a non-rotor aircraft.

    会员根据权利要求1配置翼,翼飞机。

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  • The airfoil member according to claim 1, configured as a rotor blade for a helicopter.

    会员根据权利要求1配置转子叶片直升机

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  • The various design parameters are introduced before moving on to a six-segment airfoil.

    设计参数介绍转学至部分机翼。

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  • You can specify wing attributes including camber and centerline sheeting of an airfoil.

    能够标示翅膀归结包括凸形机翼中心线护墙板

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  • Researching the adaptation of airfoil lays the foundation for designing adaptive wings.

    二维型自适应研究设计自适应机翼基础

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  • The high speed airfoil type wind turbine has the highest efficiency in high wind speeds.

    高速机翼轮机风速下达到最高使用效率

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  • 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诊断实验研究方案

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  • The effectiveness of using plasma actuation to suppress airfoil stall separation is verified.

    验证等离子激励抑制翼型失速分离有效性

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  • The system of claim 1, further comprising an aircraft, the airfoil being coupled to the aircraft.

    系统索赔1进一步组成飞机加上正在型飞机。

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  • The system of claim 11, further comprising an aircraft, the airfoil being coupled to the aircraft.

    系统索赔11进一步组成飞机加上正在型飞机。

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  • The system of claim 16, further comprising an aircraft, the airfoil being coupled to the aircraft.

    系统索赔16进一步组成飞机加上正在型飞机。

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  • Direct methods are based on the design-by-analysis approach in which the airfoil shape is specified first.

    直接方法基于设计逐案分析方法机翼形状指定第一。

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  • 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使用一个特殊翼型设计达到非常扬程失速速度强度高。

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  • The Web version of the code allows for the prescription of the inviscid velocity distribution about the airfoil.

    网上代码允许处方速度分布翼型

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  • To put the method in some perspective, it helpful to briefly outline the two general approaches to airfoil design.

    一些观点方法有助于扼要介绍两个一般方式翼型设计。

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  • 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,对于俯仰运动随着厚度减小平均阻力系数也变小。

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  • 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,对于俯仰运动随着厚度减小平均阻力系数也变小。

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