飞机模型中襟翼喷射飞机模型的漩涡分析检测方案(粒子图像测速)
检测样品
其他
检测项目
襟翼喷射飞机模型的漩涡分析
关联设备
共2种
下载方案
方案详情文
The wake behind a simpli¯ed model of a generic aircraft (the SWIM model) is measured
in the Low Speed Low turbulence wind tunnel (LSL) at Delft University of Technology.
Two measurement techniques have been used in order to qualitatively and quantitatively
measure the wake, i.e. stereoscopic particle image velocimetry (Stereo PIV) and a 5 hole
probe (5HP). Furthermore balance measurements have been carried out over a range of
con¯gurations for later comparison purposes. The goal of the wake measurements is to
give a comparison between the two measurement techniques.
The 5HP measurements are processed using a windows based program called Pressure
Field Visualisation. This program calculates vector ¯elds from the input pressure data
and has several exporting options. The Stereo PIV measurements are correlated using
DaVis 7.3 using a window size of 16 x 16 pixels with 50% overlap.
北京欧兰科技发展有限公司为您提供《飞机模型中襟翼喷射飞机模型的漩涡分析检测方案(粒子图像测速)》,该方案主要用于其他中襟翼喷射飞机模型的漩涡分析检测,参考标准《暂无》,《飞机模型中襟翼喷射飞机模型的漩涡分析检测方案(粒子图像测速)》用到的仪器有德国LaVision PIV/PLIF粒子成像测速场仪、三维立体PIV。
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