The DSMC simulation of low density flow field in small nozzle

Guobiao Cai; Huiyu Wang; Guojun Zu; Zhenpeng Zhang

The DSMC simulation of low density flow field in small nozzle

Guobiao Cai^*
, Huiyu Wang
, Guojun Zu
, Zhenpeng Zhang

^*此作品的通讯作者

宇航学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

The axial symmetric low density flow field of small nozzle is simulated numerically by using DSMC method. The results conform well with ones by differential solving N-S equations. This work has deep background of engineering application and is very imporuant to the situation controlling rocket motor design for communication satellites and space stations.

源语言	英语
页（从-至）	X-13
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	17
期	5
出版状态	已出版 - 1996

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@article{186d4d63a5174da888b702a0ff35ef7e,

title = "The DSMC simulation of low density flow field in small nozzle",

abstract = "The axial symmetric low density flow field of small nozzle is simulated numerically by using DSMC method. The results conform well with ones by differential solving N-S equations. This work has deep background of engineering application and is very imporuant to the situation controlling rocket motor design for communication satellites and space stations.",

keywords = "Flow distribution, Low density flow, Monte Carlo method, Nozzme Flow, Numerical Simulation",

author = "Guobiao Cai and Huiyu Wang and Guojun Zu and Zhenpeng Zhang",

year = "1996",

language = "英语",

volume = "17",

pages = "X--13",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "5",

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TY - JOUR

T1 - The DSMC simulation of low density flow field in small nozzle

AU - Cai, Guobiao

AU - Wang, Huiyu

AU - Zu, Guojun

AU - Zhang, Zhenpeng

PY - 1996

Y1 - 1996

N2 - The axial symmetric low density flow field of small nozzle is simulated numerically by using DSMC method. The results conform well with ones by differential solving N-S equations. This work has deep background of engineering application and is very imporuant to the situation controlling rocket motor design for communication satellites and space stations.

AB - The axial symmetric low density flow field of small nozzle is simulated numerically by using DSMC method. The results conform well with ones by differential solving N-S equations. This work has deep background of engineering application and is very imporuant to the situation controlling rocket motor design for communication satellites and space stations.

KW - Flow distribution

KW - Low density flow

KW - Monte Carlo method

KW - Nozzme Flow

KW - Numerical Simulation

UR - https://www.scopus.com/pages/publications/4243091948

M3 - 文章

AN - SCOPUS:4243091948

SN - 1001-4055

VL - 17

SP - X-13

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 5

ER -

The DSMC simulation of low density flow field in small nozzle

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