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Received: 2001-10-09

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Journal of Zhejiang University SCIENCE A 2003 Vol.4 No.1 P.35~39

http://doi.org/10.1631/jzus.2003.0035


Study of interaction between shock wave and unsteady boundary layer


Author(s):  DONG Zhi-yong, HAN Zhao-yuan

Affiliation(s):  Faculty of Civil and Architectural Engineering, Zhejiang University of Technology, Hangzhou 310014, China; more

Corresponding email(s):   dongzy@mail.hz.zj.cn

Key Words:  Moving shock wave, Unsteady boundary layer, Interaction


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DONG Zhi-yong, HAN Zhao-yuan. Study of interaction between shock wave and unsteady boundary layer[J]. Journal of Zhejiang University Science A, 2003, 4(1): 35~39.

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Abstract: 
This paper reports theoretical and experimental study of a new type of interaction of a moving shock wave with an unsteady boundary layer. This type of shock wave-boundary layer interaction describes a moving shock wave interaction with an unsteady boundary layer induced by another shock wave and a rarefaction wave. So it is different from the interaction of a stationary shock wave with steady boundary layer, also different from the interaction of a reflected moving shock wave at the end of a shock tube with unsteady boundary layer induced by an incident shock. Geometrical shock dynamics is used for the theoretical analysis of the shock wave-unsteady boundary layer interaction, and a double-driver shock tube with a rarefaction wave bursting diaphragm is used for the experimental investigation in this work.

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Reference

[1]Dong,Z.Y. and Han,Z.Y., 2000. An experimental technique of diaphragm bursting by rarefaction wave in double driver shock tube, Chinese Quarterly of Mechanics, 21(4): 427-431(in Chinese).

[2]Dong,Z.Y. and Han,Z.Y., 2002. A new type of interaction of a moving shock with an unsteady boundary layer, Chinese Quarterly of Mechanics, 23(1): 44-49(in Chinese).

[3]Han,Z.Y., Wang,Z.Q. and Yin,X.Z., 1986. An experimental technique of electrically controlled double driver shock tube for studying head-on interaction of a moving shock with a bow shock. Acta Aero. Sinica, 4(4): 394-400(in Chinese).

[4]Han,Z.Y., Wang,Z.Q. and Yin,X.Z., 1985. A method for performing oblique shock-bow shock interaction in a double driver shock tube(tunnel). Proc.15th Int. Symp. on Shock Waves. Berkeley, USA, p.533-540.

[5]Han,Z.Y. and Yin,X.Z.,1989a. Two-dimensional equations of shock dynamics for a moving gas ahead of a shock wave. Science in China, Ser A, 19(4): 369-378(in Chinese).

[6]Han,Z.Y. and Yin,X.Z., 1989b. Three-dimensional equations of shock dynamics for a moving gas ahead of a shock wave. Proc. 17th Int. Sypm. on Shock Waves and Shock Tube, Lehigh, USA, p.9-21.

[7]Han, Z.Y.,1991. Shock dynamics description of reflected wave. Proc.18th Int. Sypm. on Shock Waves,Sendai Japan, p.299-304.

[8]Han,Z.Y. and Yin,X.Z.,1993. Shock Dyamics, Kluwer Axademic Publishers/Science Press.

[9]Ruetenik,J.R. and Lemek,B,1966. Study of blast-shock interaction in a shock tube and shock tunnel, AIAA paper p.409-412.

[10]Yang,J.M.,Han, Z.Y. and Yin,X.Z., 1993. A new combination facility for testing refraction, diffraction and interaction of shock waves. Science in China, Ser.A, 23(7):954-959(in Chinese).

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