Weak shock reflection from an open end of a tube with a baffle plate

Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science

Volumn 217, Issue 6, 2003, Pages 651-660

  Kim, H D ^a   Kweon, Y H ^a   Setoguchi, T ^b   Aoki, T ^c  

^a Andong National University   (South Korea)

^b SAGA UNIVERSITY   (Japan)

^c KYUSHU UNIVERSITY   (Japan)

Author keywords

Compressible flow; Impulsive noise; Open end correction; Shock tube; Shock wave discharge; Unsteady flow

Indexed keywords

COMPRESSIBLE FLOW; COMPUTATIONAL METHODS; REFLECTION; SHOCK TUBES; UNSTEADY FLOW;

BAFFLE PLATES;

SHOCK WAVES;

BAFFLE; COMPRESSIBLE FLOW; COMPUTATIONAL FLUID DYNAMICS; MATHEMATICAL ANALYSIS; MODELING; SHOCK WAVE; UNSTEADY FLOW;

EID: 0038374618     PISSN: 09544062     EISSN: None     Source Type: Journal    
DOI: 10.1243/095440603321919572     Document Type: Article

References (16)

1. Klingenberg, G. and Heimerl, J. M. Gun muzzle blast and flash. In Progress Astronautics and Aeronautics, AIAA Educational Series, 1992.
2. Sekine, N., Matsumura, S., Takayama, K., Onodera, O. and Itoh, K. Initiation and propagation of shock waves in the exhaust pipe of an internal combustion engine (in Japanese). Jap. Soc. Mech. Engrs J., 1988, 54(498), 527-531.
3. Kentfield, J. A. C. Nonsteady, One-Dimensional, Internal, Compressible Flows (Theory and Applications), 1993. Ch. 7 (Oxford University Press).
4. Zinn, B. T. Pulsating combustion. Trans. ASME, J. Mech. Engng, 1985, 107(8), 36-41.
5. Klingel, R. and Löffler, F. Dust collection and cleaning efficiency of a pulse jet fabric filter. Filtration and Separation, 1983, 20, 205-208.
6. Raghunathan, S., Kim, H. D. and Setoguchi, T. Impulse noise and its control. Prog. Aerospace Sci., 1998, 34(1), 1-44.
7. Fox, J. A. and Vardy, A. E. The generation and alleviation of air pressure transients caused by the high speed passage of vehicles through tunnels. In Proceedings of 1st International Symposium on Aerodynamics and Ventilation of Vehicle Tunnels, 1973, G3.49-G3.64.
8. Ozawa, S., Maeda, T., Matsumura, T., Uchida, K., Kajiyama, H. and Tanemoto, K. Countermeasures to reduce micro-pressure waves radiating from exits of Shinkansen tunnels. In Proceedings of 7th International Symposium on The Aerodynamics and Ventilation of Vehicle Tunnels, Brighton, Sussex, November 1991.
9. Ozawa, S. Studies of micro-pressure wave radiated from a tunnel exit (in Japanese). Railway Technical Research Report or Japanese National Railways, 1979, Vol. 1121, pp. 1-92.
10. Moritoh, Y., Zenda, Y., Shimizu, Y. and Nagakura, K. Aerodynamic noise of high-speed railway cars. In International Conference on Speedup, 1993.
11. Rudinger, G. On the reflection of shock waves from an open end of a duct. J. App. Physics, 1955, 26(8), 981-993.
12. Rudinger, G. The reflection of pressure wave of finite amplitude from an open end of a duct. J. Fluid Mechanics, 1957, 3(1), 48-66.
13. Yee, H. C. Upwind and symmetric shock capturing schemes. NASA TM-9464, 1987.
14. Sod, G. A. A numerical study of a converging cylindrical shock. J. Fluid Mechanics, 1977, 83, 785-794.
15. Kim, H. D., Setoguchi, T., Kweon, Y. H., Miura, S. and Kashimura, H. Studies on reflection of weak shock waves from an open end of a tube with baffle plate. In 11th International Symposium on Transport Phenomena (ISTP-11), 1998, 94-99.
16. Kim, H. D. and Setoguchi, T. Study of the discharge of weak shocks from an open end of a duct. J. Sound Vibr., 1999, 226(5), 1011-1028.