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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
JoVE Journal
Engineering
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JoVE Journal
Engineering
Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
Please note that all translations are automatically generated.
Click here for the English version.
基于流动可视化方法的三角洲机翼流动结构实验研究
DOI:
10.3791/57244-v
•
09:17 min
•
April 23, 2018
•
Lu Shen
,
Zong-nan Chen
,
Chihyung Wen
1
Department of Mechanical Engineering
,
Hong Kong Polytechnic University
Chapters
00:05
Title
00:47
Wind Tunnel Setup
01:21
Set up the Laser Sheet
03:21
Camera Setup
04:04
Improved Smoke Flow Visualization
05:08
Particle Image Velocimetry Measurement
06:48
Results: Leading-edge Vortex Structures of a Delta Wing using Smoke Flow Visualization and Particle Image Velocimetry
08:34
Conclusion
Summary
Automatic Translation
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Automatic Translation
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。
Tags
Delta Wing
Flow Visualization
Leading Edge Vortex
Vortical Flow
Wind Tunnel
Particle Image Velocimetry
Smoke Flow Visualization
Laser Sheet
Optical Setup
Calibration Target Plate
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