wind tunnel testing的例句大全

Therefore, designers and researchers must place heavy reliance on wind tunnel testing of aeroelastic models.

因而设计者和研究者必须高度依赖气动弹性模型风洞试验.

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The error analysis for wind tunnel testing data

风洞实验数据误差分析

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During 1982 to 1984, the LEST Foundation finished the possibility research, made a conceptional telescope design, carried out the experiments of helium filling and wind tunnel testing for the telescope tube and suggested a detailed financial budget with a total amount of 25 million US dollars.

自1982年到1984年，LEST基金会完成了可行性研究、方案设计，做了镜筒充氦和风洞试验，并提出了一个总额为2500万美元的财政预算。

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Research of Wind Tunnel Testing Technique for Model of Van Body Truck

厢式载货汽车模型风洞试验技术的研究

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this paper shows the wind tunnel testing results of naca four symmetrical airfoil section cascades of wells turbine for wave energy conversion.

本文介绍用于波能转换的威尔斯涡轮的NACA四位数对称叶型叶栅的风洞试验结果。

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the reliability of applied formula is verified by the full-scale aero-elastic model in wind tunnel testing.

最后通过气弹模型风洞试验验证了公式的可靠性。

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Extensive testing was carried out, including wind tunnel testing as used by actual F 1 cars.

广泛的测试进行, 其中包括风洞试验所用的实际F1赛车.

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In particular, wind tunnel testing has become a useful and practical tool in these endeavors.

特别是, 风洞测试已经成为一个有用的和实用的工具在这些努力.

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The error of wind tunnel testing data and its calculating methods

风洞实验数据的误差及其计算方法

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The layout of developing the large dimension wind tunnel, high Reynolds number wind tunnel, high-energy facility, will improve the simulative ability of wind tunnel and enhance the testing level.

规划中大尺寸风洞、高雷诺数风洞、高能量气动设备的研制，将使风洞模拟能力和测试水平实现新的飞跃。

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in this paper, the testing study of a type of parafoil's aerodynamic moment characteristics in cardc 8m × 6m low speed wind tunnel is introduced.

本文介绍在8m×6m低速风洞中进行的某研究型冲压式翼平力矩特性试验研究。

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Due to the existence of boundary layer on a test floor, the characteristics of experimental flow field is different from the real situation, which leads to the inaccuracy of testing data. Therefore, the control of boundary layer is essential to a wind tunnel test floor.

由于地板附面层的存在，实验流场特征与真实情况存在差异，对实验结果的准确性产生一定影响，因而附面层的控制对风洞试验地板至关重要。

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Recently, the wide-range six-component force/ torque sensor becomes the urgent need high-tech product, which can be used in thrust testing of rocket engines, flight testing of airplane, testing of spacecraft docking simulation and wind tunnel.

近年来，应用于火箭发动机推力试验、飞机试飞试验、航天器对接模拟试验及风洞试验等领域的大量程六维力传感器，成为急需的高科技产品。

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TESTING A Wind Tunnel Study on Iron Ore Dust Pollution

铁矿粉尘污染的试验研究

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an analysis of data accuracy of force measurement testing with tps in 2.4m transonic wind tunnel

2.4m跨声速风洞带TPS测力试验数据精度要求分析

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pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel

在高速风洞中使用荧光压力传感器技术对飞机模型压力场的实验研究

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