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CLC number: O359
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Received: 2000-05-12
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RESEARCH ON DISTURBANCE PROPERTIES OF SUSPENSIONS NEAR THE INJECTION AREA OF MOVING JET
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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.
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