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Visualization of pre-set vortices in boundary layer flow over wavy surface in rectangular channel

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Abstract

Smoke-wire flow visualization is used to study the development of pre-set counter-rotating streamwise vortices in boundary layer flow over a wavy surface in a rectangular channel. The formation of the vortices is indicated by the vortical structures on the cross-sectional plane normal to the wavy surface. To obtain uniform spanwise vortex wavelength which will result in uniform vortex size, two types of spanwise disturbances were used: a series of perturbation wires placed prior and normal to the leading edge of the wavy surface, and a jagged pattern in the form of uniform triangles cut at the leading edge. These perturbation wires and jagged pattern induce low-velocity streaks that result in the formation of counter-rotating streamwise vortices that evolve downstream to form the mushroom-like structures on the cross-sectional plane of the flow. The evolution of the most amplified disturbances can be attributed to the formation of these mushroom-like structures. It is also shown that the size of the mushroom-like structures depends on the channel entrance geometry, Reynolds number, and the channel gap.

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Acknowledgments

The authors would like to express their sincere gratitude to the Temasek Laboratories, National University of Singapore for the opportunity to conduct the experiments at its Aeroscience Laboratory, and also to thank Mr. Sim Lucius and Mr. M. N. Adha bin Jamaludin for their help in setting up the experimental rig and in collecting the experimental data. The first author is a recipient of NUS Research Scholarship and would also like to thank the AUN/SEED-Net.

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Correspondence to A. C. Budiman.

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Budiman, A.C., Mitsudharmadi, H., Bouremel, Y. et al. Visualization of pre-set vortices in boundary layer flow over wavy surface in rectangular channel. J Vis 18, 669–677 (2015). https://doi.org/10.1007/s12650-014-0252-z

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  • DOI: https://doi.org/10.1007/s12650-014-0252-z

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