Numerical modeling of heat transfer and flow in low power arcjet thruster

Hai Xing Wang; Shao Xia Jia; Xi Chen; Wenxia Pan

doi:10.1063/1.3452167

Numerical modeling of heat transfer and flow in low power arcjet thruster

Hai Xing Wang^*
, Shao Xia Jia
, Xi Chen
, Wenxia Pan

^*Corresponding author for this work

School of Astronautics

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

Modeling studies are preformed to investigate the plasma and heat transfer characteristics of a low power argon arcjet thruster. Computed temperature, velocity, static pressure, and Mach number distribution in arcjet thruster under typical operating condition are presented in this paper. It shows that the performance data from numerical modeling results are basically consistent with the experimental measured values.

Original language	English
Title of host publication	ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science
Pages	209-212
Number of pages	4
Edition	PART 1
DOIs	https://doi.org/10.1063/1.3452167
State	Published - 2010
Event	2nd International Symposium on Computational Mechanics, ISCM II, and the 12th International Conference on the Enhancement and Promotion of Computational Methods in Engineering and Science, EPMESC XII - Hong Kong, Macau, China Duration: 30 Nov 2009 → 3 Dec 2009

Publication series

Name	AIP Conference Proceedings
Number	PART 1
Volume	1233
ISSN (Print)	0094-243X
ISSN (Electronic)	1551-7616

Conference

Conference	2nd International Symposium on Computational Mechanics, ISCM II, and the 12th International Conference on the Enhancement and Promotion of Computational Methods in Engineering and Science, EPMESC XII
Country/Territory	China
City	Hong Kong, Macau
Period	30/11/09 → 3/12/09

Keywords

Arcjet
Fluid Flow
Heat Transfer
Numerical Modeling

Access to Document

10.1063/1.3452167

Cite this

Wang, H. X., Jia, S. X., Chen, X., & Pan, W. (2010). Numerical modeling of heat transfer and flow in low power arcjet thruster. In ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science (PART 1 ed., pp. 209-212). (AIP Conference Proceedings; Vol. 1233, No. PART 1). https://doi.org/10.1063/1.3452167

Wang, Hai Xing ; Jia, Shao Xia ; Chen, Xi et al. / Numerical modeling of heat transfer and flow in low power arcjet thruster. ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science. PART 1. ed. 2010. pp. 209-212 (AIP Conference Proceedings; PART 1).

@inproceedings{b45d7725d7ca40c98b87979195f65629,

title = "Numerical modeling of heat transfer and flow in low power arcjet thruster",

abstract = "Modeling studies are preformed to investigate the plasma and heat transfer characteristics of a low power argon arcjet thruster. Computed temperature, velocity, static pressure, and Mach number distribution in arcjet thruster under typical operating condition are presented in this paper. It shows that the performance data from numerical modeling results are basically consistent with the experimental measured values.",

keywords = "Arcjet, Fluid Flow, Heat Transfer, Numerical Modeling",

author = "Wang, \{Hai Xing\} and Jia, \{Shao Xia\} and Xi Chen and Wenxia Pan",

year = "2010",

doi = "10.1063/1.3452167",

language = "英语",

isbn = "9780735407787",

series = "AIP Conference Proceedings",

number = "PART 1",

pages = "209--212",

booktitle = "ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science",

edition = "PART 1",

note = "2nd International Symposium on Computational Mechanics, ISCM II, and the 12th International Conference on the Enhancement and Promotion of Computational Methods in Engineering and Science, EPMESC XII ; Conference date: 30-11-2009 Through 03-12-2009",

}

Wang, HX, Jia, SX, Chen, X & Pan, W 2010, Numerical modeling of heat transfer and flow in low power arcjet thruster. in ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science. PART 1 edn, AIP Conference Proceedings, no. PART 1, vol. 1233, pp. 209-212, 2nd International Symposium on Computational Mechanics, ISCM II, and the 12th International Conference on the Enhancement and Promotion of Computational Methods in Engineering and Science, EPMESC XII, Hong Kong, Macau, China, 30/11/09. https://doi.org/10.1063/1.3452167

Numerical modeling of heat transfer and flow in low power arcjet thruster. / Wang, Hai Xing; Jia, Shao Xia; Chen, Xi et al.
ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science. PART 1. ed. 2010. p. 209-212 (AIP Conference Proceedings; Vol. 1233, No. PART 1).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Numerical modeling of heat transfer and flow in low power arcjet thruster

AU - Wang, Hai Xing

AU - Jia, Shao Xia

AU - Chen, Xi

AU - Pan, Wenxia

PY - 2010

Y1 - 2010

N2 - Modeling studies are preformed to investigate the plasma and heat transfer characteristics of a low power argon arcjet thruster. Computed temperature, velocity, static pressure, and Mach number distribution in arcjet thruster under typical operating condition are presented in this paper. It shows that the performance data from numerical modeling results are basically consistent with the experimental measured values.

AB - Modeling studies are preformed to investigate the plasma and heat transfer characteristics of a low power argon arcjet thruster. Computed temperature, velocity, static pressure, and Mach number distribution in arcjet thruster under typical operating condition are presented in this paper. It shows that the performance data from numerical modeling results are basically consistent with the experimental measured values.

KW - Arcjet

KW - Fluid Flow

KW - Heat Transfer

KW - Numerical Modeling

UR - https://www.scopus.com/pages/publications/77955731480

U2 - 10.1063/1.3452167

DO - 10.1063/1.3452167

M3 - 会议稿件

AN - SCOPUS:77955731480

SN - 9780735407787

T3 - AIP Conference Proceedings

SP - 209

EP - 212

BT - ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science

T2 - 2nd International Symposium on Computational Mechanics, ISCM II, and the 12th International Conference on the Enhancement and Promotion of Computational Methods in Engineering and Science, EPMESC XII

Y2 - 30 November 2009 through 3 December 2009

ER -

Wang HX, Jia SX, Chen X, Pan W. Numerical modeling of heat transfer and flow in low power arcjet thruster. In ISCM II and EPMESC XII - Proc. of the 2nd Int. Symposium on Computational Mechanics and the 12th Int. Conf. on the Enhancement and Promotion of Computational Methods in Engineering and Science. PART 1 ed. 2010. p. 209-212. (AIP Conference Proceedings; PART 1). doi: 10.1063/1.3452167

Numerical modeling of heat transfer and flow in low power arcjet thruster

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