Abstract
The current work presents the results of an experimental study using a conventional diaphragm-constrained, air-driven, circular cross-section shock tube expanding into ambient conditions producing shockMach numbers between 1.25 and 1.64.
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Abe, A., Watanabe, M.: Three dimensional flow structure behind a shock wave discharged from a rectangular cross section shock tube. In: Takayama, K. (ed.) Shock Waves: Proceedings of the 18th International Symposium, Sendai, Japan, July 21-26, pp. 209–212. Springer (1991)
Brouillette, M., Hébert, C.: Propagation and interaction of shock-generated vortices. Fluid Dyn. Res. 21(3), 159–169 (1997)
Elder, F.K., De Haas, N.: Experimental study of the formation of a vortex ring at the open end of a cylindrical shock tube. J. Appl. Phys. 23(10), 1065–1069 (1952)
Jiang, Z., Onodera, O., Takayama, K.: Evolution of shock waves and the primary vortex loop discharged from a square cross-sectional tube. Shock Waves 9(1), 1–10 (1999)
Kim, H.-D., Kweon, Y.-H., Setoguchi, T.: A study of the impulsive wave discharged from the inclined exit of a tube. P I Mech. Eng. C-J Mec. 217, 271–279 (2003)
Kleine, H., Vo Le, C., Takehara, K., Etoh, T.G.: Time-resolved visualization of shock-vortex systems emitted from an open shock tube. J. Visual-Japan 13(1), 33–40 (2009)
Zare-Behtash, H., Kontis, K., Gongora-Orozco, N., Takayama, K.: Shock wave-induced vortex loops emanating from nozzles with singular corners. Exp. Fluids 49(5), 1005–1019 (2010)
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Paton, R.T., Skews, B.W. (2015). Shock Wave Diffraction at the Inclined Exit of a Shock Tube. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 2. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16838-8_78
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DOI: https://doi.org/10.1007/978-3-319-16838-8_78
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-16837-1
Online ISBN: 978-3-319-16838-8
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