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Journal / Engineering / 基于流动可视化方法的三角洲机翼流动结构实验研究…
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基于流动可视化方法的三角洲机翼流动结构实验研究
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基于流动可视化方法的三角洲机翼流动结构实验研究

Article DOI: 10.3791/57244-v • 09:17 min • April 23rd, 2018
April 23rd, 2018 •
1, 1, 1
1Department of Mechanical Engineering, Hong Kong Polytechnic University

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在这里, 我们提出了一种通过改进的烟雾流可视化技术来观察三角洲机翼上非恒定涡流流的协议, 并研究了导致前缘涡击穿位置振荡的机制。

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工程 问题 134 三角洲机翼 烟雾流动可视化 前缘涡 涡击穿 涡流振荡 粒子图像测速仪
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