Graphic abstract
This is a preview of subscription content, log in via an institution to check access.
References
Babinsky H, Harvey JK (2011) Shock wave-boundary-layer interactions, vol 32. Cambridge University Press, Cambridge
Billig F, Kothari A (2000) Streamline tracing: technique for designing hypersonic vehicles. J Propul Power 16(3):465–471. https://doi.org/10.2514/2.5591
He G, Zhou J, Zhao YX (2018) Application of free interaction theory in swept shock wave/turbulent boundary layer interactions. J Vis 21(2):203–214
Knight DD, Horstman C, Bogdonoff S (1992) Structure of supersonic turbulent flow past a swept compression corner. AIAA J 30(4):890–896
Molder S, Szpiro EJ (1966) Busemann inlet for hypersonic speeds. J Spacecr Rockets 3(8):1172–1176
Sheng FJ, Tan HJ, Zhuang Y, Huang HX, Chen H, Wang WX (2018) Visualization of conical vortex and shock in swept shock/turbulent boundary layer interaction flow. J Vis 21(6):909–914
Smith MW, Smits AJ (1995) Visualization of the structure of supersonic turbulent boundary layer. Exp Fluids 18(4):288–302
Zhao YX, Yi SH, Tian LF, Cheng ZY (2009) Supersonic flow imaging via nanoparticles. Sci China Ser E: Technol Sci 52(12):3640–3648. https://doi.org/10.1007/s11431-009-0281-3
Zhuang Y, Tan HJ, Li X, Sheng FJ, Zhang YC (2018) Görtler-like vortices in an impinging shock wave/turbulent boundary layer interaction flow. Phys Fluids 30(6):061702. https://doi.org/10.1063/1.5034242
Zhuang Y, Tan HJ, Wang WX, Li X, Guo YJ (2019) Fractal features of turbulent/non-turbulent interface in a shock wave/turbulent boundary-layer interaction flow. J Fluid Mech. https://doi.org/10.1017/jfm.2019.299
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.
Author information
Authors and Affiliations
Corresponding author
Additional information
Publisher's Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Rights and permissions
About this article
Cite this article
Zhang, Y., Chen, L., Tan, Hj. et al. Visualization of curved swept shock wave/turbulent boundary layer interaction in supersonic flow. J Vis 24, 1–7 (2021). https://doi.org/10.1007/s12650-020-00692-5
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s12650-020-00692-5