Stationary numerical simulation of flow separation and side load in nozzle

Ya Bing Liu; Chang Hui Wang; Xiao Yong Xu

Stationary numerical simulation of flow separation and side load in nozzle

Ya Bing Liu^*
, Chang Hui Wang
, Xiao Yong Xu

^*Corresponding author for this work

School of Astronautics

Research output: Contribution to journal › Article › peer-review

7 Scopus citations

Abstract

A three-dimensional, viscous and steady numerical simulation about serpentine flow was conducted for a high-altitude nozzle of a liquid rocket engine on the ground. The results with different inlet pressure were obtained by utilizing FLUENT software. The transformation of shock pattern and the distribution of unsymmetrical separation and side load in the nozzle were primarily predicted by those results. The simulation provides a key basis for further study.

Original language	English
Pages (from-to)	2114-2118
Number of pages	5
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	23
Issue number	11
State	Published - Nov 2008

Keywords

Flow separation
Liquid rocket engine
Nozzle
Numerical simulation
Side load

Cite this

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title = "Stationary numerical simulation of flow separation and side load in nozzle",

abstract = "A three-dimensional, viscous and steady numerical simulation about serpentine flow was conducted for a high-altitude nozzle of a liquid rocket engine on the ground. The results with different inlet pressure were obtained by utilizing FLUENT software. The transformation of shock pattern and the distribution of unsymmetrical separation and side load in the nozzle were primarily predicted by those results. The simulation provides a key basis for further study.",

keywords = "Flow separation, Liquid rocket engine, Nozzle, Numerical simulation, Side load",

author = "Liu, \{Ya Bing\} and Wang, \{Chang Hui\} and Xu, \{Xiao Yong\}",

year = "2008",

month = nov,

language = "英语",

volume = "23",

pages = "2114--2118",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

publisher = "BUAA Press",

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TY - JOUR

T1 - Stationary numerical simulation of flow separation and side load in nozzle

AU - Liu, Ya Bing

AU - Wang, Chang Hui

AU - Xu, Xiao Yong

PY - 2008/11

Y1 - 2008/11

N2 - A three-dimensional, viscous and steady numerical simulation about serpentine flow was conducted for a high-altitude nozzle of a liquid rocket engine on the ground. The results with different inlet pressure were obtained by utilizing FLUENT software. The transformation of shock pattern and the distribution of unsymmetrical separation and side load in the nozzle were primarily predicted by those results. The simulation provides a key basis for further study.

AB - A three-dimensional, viscous and steady numerical simulation about serpentine flow was conducted for a high-altitude nozzle of a liquid rocket engine on the ground. The results with different inlet pressure were obtained by utilizing FLUENT software. The transformation of shock pattern and the distribution of unsymmetrical separation and side load in the nozzle were primarily predicted by those results. The simulation provides a key basis for further study.

KW - Flow separation

KW - Liquid rocket engine

KW - Nozzle

KW - Numerical simulation

KW - Side load

UR - https://www.scopus.com/pages/publications/57449104529

M3 - 文章

AN - SCOPUS:57449104529

SN - 1000-8055

VL - 23

SP - 2114

EP - 2118

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 11

ER -

Stationary numerical simulation of flow separation and side load in nozzle

Abstract

Keywords

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