DSMC simulation of low-density flow-field in a small nozzle

Guobiao Cai; Huiyu Wang; Guojun Zu; Zhenpeng Zhang

DSMC simulation of low-density flow-field in a small nozzle

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

^*此作品的通讯作者

Peking University

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The axially symmetric low-density flow-field of a small nozzle used for changing the attitude of satellite was simulated by using the DSMC method, and the obtained results were compared with the ones from solving the N-S equations by using the differential method with good agreement. The method presented is of significance to the design of rocket motor for controlling the attitude of communication satellites and space station.

源语言	英语
页（从-至）	9-13
页数	5
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	17
期	5
出版状态	已出版 - 10月 1996
已对外发布	是

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@article{088120a62120419c863dbde01c036273,

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

abstract = "The axially symmetric low-density flow-field of a small nozzle used for changing the attitude of satellite was simulated by using the DSMC method, and the obtained results were compared with the ones from solving the N-S equations by using the differential method with good agreement. The method presented is of significance to the design of rocket motor for controlling the attitude of communication satellites and space station.",

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

year = "1996",

month = oct,

language = "英语",

volume = "17",

pages = "9--13",

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

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publisher = "China Aerospace Science and Industry Corp",

number = "5",

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TY - JOUR

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

AU - Cai, Guobiao

AU - Wang, Huiyu

AU - Zu, Guojun

AU - Zhang, Zhenpeng

PY - 1996/10

Y1 - 1996/10

N2 - The axially symmetric low-density flow-field of a small nozzle used for changing the attitude of satellite was simulated by using the DSMC method, and the obtained results were compared with the ones from solving the N-S equations by using the differential method with good agreement. The method presented is of significance to the design of rocket motor for controlling the attitude of communication satellites and space station.

AB - The axially symmetric low-density flow-field of a small nozzle used for changing the attitude of satellite was simulated by using the DSMC method, and the obtained results were compared with the ones from solving the N-S equations by using the differential method with good agreement. The method presented is of significance to the design of rocket motor for controlling the attitude of communication satellites and space station.

UR - https://www.scopus.com/pages/publications/0030252024

M3 - 文章

AN - SCOPUS:0030252024

SN - 1001-4055

VL - 17

SP - 9

EP - 13

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 5

ER -

DSMC simulation of low-density flow-field in a small nozzle

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