Shock Wave Diffraction at the Inclined Exit of a Shock Tube
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-16838-8_78
Reference7 articles.
1. 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)
2. Brouillette, M., Hébert, C.: Propagation and interaction of shock-generated vortices. Fluid Dyn. Res. 21(3), 159–169 (1997)
3. 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)
4. 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)
5. 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)
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1. Visualisation of plane shock wave diffraction from the curved exit of a shock tube;Journal of Visualization;2014-12-27
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