首页> 外文会议>Instrumentation in Aerospace Simulation Facilities, 1999. ICIASF 99. 18th International Congress on >Application of 3 component laser-Doppler velocimetry in transonicflow over a delta wing
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Application of 3 component laser-Doppler velocimetry in transonicflow over a delta wing

机译:三分量激光多普勒测速仪在跨音速中的应用流过三角翼

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In the development of numerical codes for the prediction ofaerodynamic flows is a strong need to obtain reliable flow field datawhich is suited to validate turbulence models used in numericalcalculations. In three dimensional boundary layers Laser-DopplerVelocimetry (LDV) is the appropriate technique usually applied to obtainthis kind of data. Since LDV, being a single point measurementtechnique, is a time consuming method, it is desirable to have theability to make use of data from different experiments and researchgroups. Therefore it is necessary to have a standard to compareexperimental results obtained by different LDV processors and to definea consistent mathematical algorithm to process data from the differentLDV experiments. This is the objective of the present paper. In anEuropean activity four different research groups have conducted commonexperiments in industrial wind tunnels and finally compared the resultsto qualify LDV for the application in industrial wind tunnel and todefine a standard to compare LDV data coming from differentsources
机译:在开发用于预测的数字代码时 空气动力学流动是获得可靠流场数据的强烈需求 适合验证数值中使用的湍流模型 计算。在三维边界层中的激光多普勒 测速(LDV)是通常用于获得 这种数据。从LDV开始,是单点测量 技术,是一种耗时的方法, 利用来自不同实验和研究的数据的能力 组。因此,有必要制定一个标准进行比较 不同LDV处理器获得的实验结果,并定义 一致的数学算法来处理来自不同数据的数据 LDV实验。这是本文的目的。在 欧洲活动四个不同的研究小组进行了共同 在工业风洞中进行实验,最后比较结果 使LDV具备在工业风洞中应用的资格,并且 定义一个标准来比较来自不同地方的LDV数据 资料来源

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