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

^*Corresponding author for this work

School of Astronautics

Beihang University

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

1 Scopus citations

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.

Original language	English
Pages (from-to)	X-13
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	17
Issue number	5
State	Published - 1996

Keywords

Flow distribution
Low density flow
Monte Carlo method
Nozzme Flow
Numerical Simulation

Cite this

@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",

}

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

Abstract

Keywords

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