CLC number: O359
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
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LIN Jian-zhong, ZHOU Ze-xuan, WU Tao, YOU Zhen-jiang. RESEARCH ON DISTURBANCE PROPERTIES OF SUSPENSIONS NEAR THE INJECTION AREA OF MOVING JET[J]. Journal of Zhejiang University Science A, 2001, 2(1): 15-23.
@article{title="RESEARCH ON DISTURBANCE PROPERTIES OF SUSPENSIONS NEAR THE INJECTION AREA OF MOVING JET",
author="LIN Jian-zhong, ZHOU Ze-xuan, WU Tao, YOU Zhen-jiang",
journal="Journal of Zhejiang University Science A",
volume="2",
number="1",
pages="15-23",
year="2001",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.2001.0015"
}
%0 Journal Article
%T RESEARCH ON DISTURBANCE PROPERTIES OF SUSPENSIONS NEAR THE INJECTION AREA OF MOVING JET
%A LIN Jian-zhong
%A ZHOU Ze-xuan
%A WU Tao
%A YOU Zhen-jiang
%J Journal of Zhejiang University SCIENCE A
%V 2
%N 1
%P 15-23
%@ 1869-1951
%D 2001
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.2001.0015
TY - JOUR
T1 - RESEARCH ON DISTURBANCE PROPERTIES OF SUSPENSIONS NEAR THE INJECTION AREA OF MOVING JET
A1 - LIN Jian-zhong
A1 - ZHOU Ze-xuan
A1 - WU Tao
A1 - YOU Zhen-jiang
J0 - Journal of Zhejiang University Science A
VL - 2
IS - 1
SP - 15
EP - 23
%@ 1869-1951
Y1 - 2001
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.2001.0015
Abstract: The equation of the suspension-gas non-streamwise complex disturbance velocity ratio near the injection area of moving jet was theoretically derived by using a phase-coupled model and stability theory. Then the ratio curves were obtained by the finite difference method based on the asymptotic method and the Euler conservative difference scheme.Analysis of the curves yielded conclusions on the disturbance properties of suspensions and effects of the natures of the flow-field and the properties of the suspensions on the suspensions' ability to track the disturbed gas flow are presented in this paper.
[1] Alfons Michalke and Gunter Hermann,1982.On the instability of a circular jet with external flow.Journal of Fluid Mechanics,114:343-359.
[2] Chung,J.N.,and Troutt,T.R.,1988,Simulation of particle dispersion in an axisymmetric jet.Journal of Fluid Mechanics,186:199-222.
[3] Kong Kang,Qin Mengzhao,1991.Hamilton algorithm of hamilton dynamic system.Progress in Natural Science,(2):102-112.
[4] Lin Jianzhong,Shen Liping,Zhou Zexuan,2000.The effect of the coherent structures in the boundary layer flow on erosion.Wear,241:10-16.
[5] Logmire,E.K.,and Eaton,J.K.,1992.Structure of a particle-laden round jet.Journal of Fluid Mechanics,236:217-257.
[6] Logmire,E.K.,and Eaton,J.K.,1994.Active open-loop control of particle dispersion in round jets.AIAA.Journal,32:555-563.
[7] Peterson,R.A.,and Samet,M.M.,1988.On the preferred mode of jet instability.Journal of Fluid Mechanics,77:511-529.
[8] Ramkumar N.Parthasarathy,1995.Stability of particle-laden round jets to small disturbances.FED-Gas-Particle Flow,ASME,228:427-433.
[9] Sykes,D.,and Lyell,M.J.,1994.The effect of particle loading on the spatial stability of a circular jet.Physics of Fluids,6:1937-1939.
[10] Yang,Y.,Chung,J.N.,Troutt,T.R.,and Crowe,C.T.,1990.The influence of particles on the spatial stability of two-phase mixing layers.Physics of Fluids A,2:1839-1845.
[11] Zhou Zexuan,Lin Jianzhong,Wang Canxing et al.,1999.Disturbance property of suspensions lying on interface of moving two-phase jet.Proceedings' of 8th Asian Congress of Fluid Mechanics,Shenzhen,China,p.137-140.
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