Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system

Longxian Xue; Dong Zhu; Xuhui Wang; Dong Xiang

doi:10.1109/AUS.2016.7748206

Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system

Longxian Xue
, Dong Zhu^*
, Xuhui Wang
, Dong Xiang

^*Corresponding author for this work

China Aviation Industry Corporation
School of Mechatronics Engineering, Harbin Institute of Technology

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

Abstract

The two dimensions model of aircraft pneumatic system with constant volume tank is established, the model includes constant volume tank, orifice and pipe. The heat transfer among the air inside the pneumatic system, pneumatic components and air outside the pneumatic system is involved in the simulation. The two dimensions unsteady flow field in charging and discharging tank is calculated. After charging and discharging, the temperature of components in the system is different, the lowest temperature is the orifice's surface temperature. With the method displaced in this article, the two dimensions flow field in pneumatic system can be obtained.

Original language	English
Title of host publication	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1020-1023
Number of pages	4
ISBN (Electronic)	9781509010875
DOIs	https://doi.org/10.1109/AUS.2016.7748206
State	Published - 17 Nov 2016
Externally published	Yes
Event	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China Duration: 10 Oct 2016 → 12 Oct 2016

Publication series

Name	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

Conference

Conference	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Country/Territory	China
City	Beijing
Period	10/10/16 → 12/10/16

Keywords

charging and discharging
two dimensions
unsterdy flow field

Access to Document

10.1109/AUS.2016.7748206

Cite this

Xue, L., Zhu, D., Wang, X., & Xiang, D. (2016). Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems (pp. 1020-1023). Article 7748206 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AUS.2016.7748206

Xue, Longxian ; Zhu, Dong ; Wang, Xuhui et al. / Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system. AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 1020-1023 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

@inproceedings{da1a063f4ddc47ad8f81586a26d79d85,

title = "Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system",

abstract = "The two dimensions model of aircraft pneumatic system with constant volume tank is established, the model includes constant volume tank, orifice and pipe. The heat transfer among the air inside the pneumatic system, pneumatic components and air outside the pneumatic system is involved in the simulation. The two dimensions unsteady flow field in charging and discharging tank is calculated. After charging and discharging, the temperature of components in the system is different, the lowest temperature is the orifice's surface temperature. With the method displaced in this article, the two dimensions flow field in pneumatic system can be obtained.",

keywords = "charging and discharging, two dimensions, unsterdy flow field",

author = "Longxian Xue and Dong Zhu and Xuhui Wang and Dong Xiang",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 ; Conference date: 10-10-2016 Through 12-10-2016",

year = "2016",

month = nov,

day = "17",

doi = "10.1109/AUS.2016.7748206",

language = "英语",

series = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "1020--1023",

booktitle = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

address = "美国",

}

Xue, L, Zhu, D, Wang, X & Xiang, D 2016, Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system. in AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems., 7748206, AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, Institute of Electrical and Electronics Engineers Inc., pp. 1020-1023, 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016, Beijing, China, 10/10/16. https://doi.org/10.1109/AUS.2016.7748206

Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system. / Xue, Longxian; Zhu, Dong; Wang, Xuhui et al.
AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. p. 1020-1023 7748206 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

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

TY - GEN

T1 - Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system

AU - Xue, Longxian

AU - Zhu, Dong

AU - Wang, Xuhui

AU - Xiang, Dong

PY - 2016/11/17

Y1 - 2016/11/17

N2 - The two dimensions model of aircraft pneumatic system with constant volume tank is established, the model includes constant volume tank, orifice and pipe. The heat transfer among the air inside the pneumatic system, pneumatic components and air outside the pneumatic system is involved in the simulation. The two dimensions unsteady flow field in charging and discharging tank is calculated. After charging and discharging, the temperature of components in the system is different, the lowest temperature is the orifice's surface temperature. With the method displaced in this article, the two dimensions flow field in pneumatic system can be obtained.

AB - The two dimensions model of aircraft pneumatic system with constant volume tank is established, the model includes constant volume tank, orifice and pipe. The heat transfer among the air inside the pneumatic system, pneumatic components and air outside the pneumatic system is involved in the simulation. The two dimensions unsteady flow field in charging and discharging tank is calculated. After charging and discharging, the temperature of components in the system is different, the lowest temperature is the orifice's surface temperature. With the method displaced in this article, the two dimensions flow field in pneumatic system can be obtained.

KW - charging and discharging

KW - two dimensions

KW - unsterdy flow field

UR - https://www.scopus.com/pages/publications/85006791350

U2 - 10.1109/AUS.2016.7748206

DO - 10.1109/AUS.2016.7748206

M3 - 会议稿件

AN - SCOPUS:85006791350

T3 - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

SP - 1020

EP - 1023

BT - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016

Y2 - 10 October 2016 through 12 October 2016

ER -

Xue L, Zhu D, Wang X, Xiang D. Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc. 2016. p. 1020-1023. 7748206. (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). doi: 10.1109/AUS.2016.7748206

Numerical simulation of two-dimension unsteady flow field in aircraft pneumatic system

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