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翼型会员包括。An airfoil member comprising.

刹车是如何作用于滑翔伞的翼型?How does the brake act on the paraglider airfoil?

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仿生学单细胞虫今天宣布发型了3.3版机翼。Rogue Amoeba today announced the release of Airfoil 3.3.

在方法,这种称为翼型四个部分机翼。In the method, such an airfoil is termed a four-segment airfoil.

撑条–插入到翼布中用来固定翼型的肋骨条。BATTEN – formed rib that slips into sail to define airfoil shape.

在气动弹性力学中,机翼振颤是一个非常典型的问题。Airfoil flutter is one of the important problems in aeroelasticity.

连接机翼的前缘与后缘的直线。A straight line connecting the leading and trailing edges of an airfoil.

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光学提拉力与机翼翼面产生的空气动力不同。Optical lift is different from the aerodynamic lift created by an airfoil.

由于机翼的分析,以确定那是说,它的速度分布。The given airfoil is then analyzed to determine, say, its velocity distribution.

提出了一种有效的跨音速翼型气动优化设计方法。An effective aerodynamic optimization design method of transonic airfoil is given.

而扑动翼翼型弯度的增加不利于推力特性的提高。It is disadvantageous to thrust characteristic through increase camber of airfoil.

各设计参数介绍转学至六部分机翼。The various design parameters are introduced before moving on to a six-segment airfoil.

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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。You can specify wing attributes including camber and centerline sheeting of an 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。Provide the experimental research scheme to measure and diagnose boundary layer of airfoil.

在试验方面,利用水洞对S形翼型的绕流流场进行了实测。Experimentally, the flow-field roud the S-shaped airfoil is tested by means of a water cave.

本文首次把S形翼型作为研究对象进行理论计算和试验研究。This paper deals theoretical and experimentally with the S-shaped airfoil for the first time.

在试验结果的基础上,对叶型受感部结构进行了优化。The structure of the airfoil sensing area was optimized based on the result of the experiment.

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提出在垂直极化状态下机翼后缘绕射的计算必须将后缘厚度考虑在内的见解。The scattering peak of leading edge depends only on radius of airfoil for horizontal polarization.

进一步分析了多段翼型使用嵌套网格的粘性求解技术。The Chimera grid technique for solving viscous flow field of the multi-element airfoil was studied.

用端板法测量气动力数据时,端板附近有自由涡拖出。In the conventional airfoil tests using, end-plates, the free vortex may be drawn around end-plates.