Simulation Analysis of Two-Phase Flow in Fluid Throat of Burner for Thermal Fatigue Testing

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

Abstract

To address the issue of testing single component under multiple working conditions in thermal fatigue tests of aircraft engine parts, it is of great significance to regulate the pressure inside the combustor by injecting secondary flow at the throat of the combustor. In this paper, a discrete phase model (DPM) of water is introduced to simulate the gas-liquid two-phase flow field at the throat of the combustor. The effects of water, water vapor, and two-phase flow of water and water vapor on pressure regulation are compared, and the basic rules of jet flow rate and angle on pressure regulation are analyzed, providing guidance for thermal machine fatigue tests and greatly reducing test costs. This work provides a new approach for combustor adaptive pressure regulation.

Original languageEnglish
Title of host publicationMechanical and Aerospace Engineering - Proceedings of the 15th International Conference, ICMAE 2024
EditorsPasquale Daponte
PublisherIOS Press BV
Pages422-434
Number of pages13
ISBN (Electronic)9781643685984
DOIs
StatePublished - 16 Jun 2025
Event15th International Conference on Mechanical and Aerospace Engineering, ICMAE 2024 - Zagreb, Croatia
Duration: 17 Jul 202420 Jul 2024

Publication series

NameAdvances in Transdisciplinary Engineering
Volume71
ISSN (Print)2352-751X
ISSN (Electronic)2352-7528

Conference

Conference15th International Conference on Mechanical and Aerospace Engineering, ICMAE 2024
Country/TerritoryCroatia
CityZagreb
Period17/07/2420/07/24

Keywords

  • DPM model
  • Thermal machine fatigue
  • fluid throat
  • gas-liquid two phase flow

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