CLC number: O354.5
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 0000-00-00
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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.
@article{title="Study of interaction between shock wave and unsteady boundary layer",
author="DONG Zhi-yong, HAN Zhao-yuan",
journal="Journal of Zhejiang University Science A",
volume="4",
number="1",
pages="35-39",
year="2003",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.2003.0035"
}
%0 Journal Article
%T Study of interaction between shock wave and unsteady boundary layer
%A DONG Zhi-yong
%A HAN Zhao-yuan
%J Journal of Zhejiang University SCIENCE A
%V 4
%N 1
%P 35-39
%@ 1869-1951
%D 2003
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.2003.0035
TY - JOUR
T1 - Study of interaction between shock wave and unsteady boundary layer
A1 - DONG Zhi-yong
A1 - HAN Zhao-yuan
J0 - Journal of Zhejiang University Science A
VL - 4
IS - 1
SP - 35
EP - 39
%@ 1869-1951
Y1 - 2003
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.2003.0035
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.
[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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