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This student research project deals with the investigations of the flow phenomena over a
three dimensional moving airfoil. The complex motion apparatus was set up to create a
pitching, plunging and rolling movement of a two dimensional wind tunnel model. The main
objective was to determine the position of transition with respect to the phase angle and
span-wise distribution. The campaign focussed Stereo PIV measurements, but also Mini
Tuft-, Oilfilm- and SSLCC- Techniques, contributed to the results. It can be shown that the
flow field is not dominated by side-wall effects, while the transition oscillates corresponding
to the spanwise variation of the heaving cycle.
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北京欧兰科技发展有限公司为您提供《翼型中平移边界层立体PIV测量检测方案(粒子图像测速)》，该方案主要用于其他中平移边界层立体PIV测量检测，参考标准《暂无》，《翼型中平移边界层立体PIV测量检测方案(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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