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

^*此作品的通讯作者

宇航学院

Beihang University
Beijing Power Machinery Research Institute

科研成果: 期刊稿件 › 文章 › 同行评审

7 引用（Scopus）

摘要

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.

源语言	英语
页（从-至）	2114-2118
页数	5
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	23
期	11
出版状态	已出版 - 11月 2008

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引用此

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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",

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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

摘要

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