How does the brake act on the paraglider airfoil?
刹车是如何作用于滑翔伞的机翼的？
Airfoil design technology and criterion are investigated.
进行了叶型设计技术和准则的研究。
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。
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。
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。
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。
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。
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。
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。
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。
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。
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。
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。
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。
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。
The interior of the airfoil is then mapped onto an infinite strip in the complex potential plane.
翼型的内部在复位势平面中可转绘成无限长的条带。
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。
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。
The control of flow on YLSG107 airfoil using synthetic jet actuator is investigated experimentally.
进行了合成射流用于YLSG107翼型流动控制的实验尝试。
The ice accretion geometric characteristics have complex effects on airfoil aerodynamic coefficients.
积冰几何形状对翼型气动系数的影响是复杂的。
The control of supercritical airfoil boundary layer separation is adapted using micro-vortex generators.
超临界翼型附面层分离控制适合采用微型涡流发生器。
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。
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。
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。
The instrumentation and experimental method of low-speed airfoil dynamic study are presented briefly in this paper.
简述了翼型低速动态实验研究的测试设备和实验方法。
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
The variable-domain variation is a specific tool of handling unknown boundaries and suitable for designing airfoil shape.
变域变分是一种处理未知界面的独特工具，极适合于气动外形的设计求解。
The variable-domain variation is a specific tool of handling unknown boundaries and suitable for designing airfoil shape.
变域变分是一种处理未知界面的独特工具，极适合于气动外形的设计求解。
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