Visualization of curved swept shock wave/turbulent boundary layer interaction in supersonic flow

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Acknowledgments

This work is funded by the National Nature Science Foundation of P. R. China through Grant Nos. 51806102, 11532007 and the priority academic program development of Jiangsu higher education institutions.

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Correspondence to Yue Zhang.

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Zhang, Y., Chen, L., Tan, H. et al. Visualization of curved swept shock wave/turbulent boundary layer interaction in supersonic flow. J Vis (2020). https://doi.org/10.1007/s12650-020-00692-5

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