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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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Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
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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

DOI:
10.3791/57244-v

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09:17 min

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April 23, 2018

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, ,
1Department of Mechanical Engineering,Hong Kong Polytechnic University

Capítulos

  • 00:05Título
  • 00:47Wind Tunnel Setup
  • 01:21Set up the Laser Sheet
  • 03:21Camera Setup
  • 04:04Improved Smoke Flow Visualization
  • 05:08Particle Image Velocimetry Measurement
  • 06:48Results: Leading-edge Vortex Structures of a Delta Wing using Smoke Flow Visualization and Particle Image Velocimetry
  • 08:34Conclusion

Summary

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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。

Tags

Delta WingFlow VisualizationLeading Edge VortexVortical FlowWind TunnelParticle Image VelocimetrySmoke Flow VisualizationLaser SheetOptical SetupCalibration Target Plate

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