Aerodynamic modeling and transient performance improvement of a free jet altitude test facility

Feng Wu, Limin Gao, Xinyun Wu, Xudong Feng, Lintao Leng, Yaoyu Li

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Scopus citations

Abstract

An inlet-engine altitude test facility for flight condition simulation is modeled for the system dynamic performance improvement. The system model equations are solved with an improved Euler integral method. To simulate the interaction between the tested engine and the test bench accurately, a turbojet engine module is introduced in the system model. By modeling and simulation, a linear temperature compensation control algorithm based on the control error is validated for feasibility; controller parameters optimization for cabin static pressure stabilizing is also carried out. In this paper, some issues like temperature transient performance and engine operate impact restraint on cabin static pressure are discussed efficiently and economically. With the characteristics of high efficiency and economy, the modeling and simulation tools are suitable for the optimization of such systems.

Original languageEnglish
Title of host publicationArtificial Intelligence and Security - 6th International Conference, ICAIS 2020, Proceedings
EditorsXingming Sun, Jinwei Wang, Elisa Bertino
PublisherSpringer Science and Business Media Deutschland GmbH
Pages618-630
Number of pages13
ISBN (Print)9789811581007
DOIs
StatePublished - 2020
Event6th International Conference on Artificial Intelligence and Security,ICAIS 2020 - Hohhot, China
Duration: 17 Jul 202020 Jul 2020

Publication series

NameCommunications in Computer and Information Science
Volume1254 CCIS
ISSN (Print)1865-0929
ISSN (Electronic)1865-0937

Conference

Conference6th International Conference on Artificial Intelligence and Security,ICAIS 2020
Country/TerritoryChina
CityHohhot
Period17/07/2020/07/20

Keywords

  • Aerodynamic modeling
  • ATF
  • Transient performance improvement

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