Title
A Multi-Cavity Iterative Modeling Method for the Exhaust Systems of Altitude Ground Test Facilities
Abstract
To solve the modeling problem of altitude ground test facility (AGTF) exhaust systems, which is caused by nonlinearity along the gas path and the difficulty of ejection factor calculation, a multi-cavity iterative modeling method is presented. The components of exhaust systems, such as the exhaust diffuser and cooler, are built with a series of volumes. It overcomes the disadvantage that traditional lumped-parameter models have, whereby they cannot calculate the dynamic parameters along the gas path. The exhaust system model is built with an iterative method based on multi-cavity components, and simulations are carried out under experimental conditions. The simulation results show that the maximum error of pressure is 2 kPa in the steady state and less than 6 kPa in the transient process compared with experimental data. Closed-loop simulations are also carried out to further verify the accuracy and effectiveness of the multi-cavity iterative exhaust system modeling method.
Year
DOI
Venue
2022
10.3390/sym14071399
SYMMETRY-BASEL
Keywords
DocType
Volume
altitude ground test facility, exhaust system, multi-cavity iterative model
Journal
14
Issue
ISSN
Citations 
7
2073-8994
0
PageRank 
References 
Authors
0.34
0
10
Name
Order
Citations
PageRank
Keqiang Miao101.35
Xi Wang202.37
Meiyin Zhu301.69
Song Zhang400.68
Zhihong Dan500.34
Jiashuai Liu601.35
Shubo Yang702.03
Xitong Pei801.01
Xin Wang9018.25
Louyue Zhang1001.01