Steady-State Stress Prediction of Engine Components Using the State Function Method

Wei Wang, Zhufeng Yue, Junfeng Zhang, Yixiong Liu, Yunwu Wu

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

Abstract

In order to obtain the steady-state stress of the critical component for engine preliminary design, this paper performs a comprehensive investigation on the stress estimation using the proposed state function method. The basic principle is the implementation of the engine similarity criteria. To be specific, the steady-state temperature and stress fields of engine components are solely functions of height (H), Mach number (Ma), and rotational speed (N) for the specified engine. Therefore, it is possible to accurately determine the temperature and stress of the components under the desired operating condition. Four coefficients need to be calculated using the sampling points. Results show that the predicted stress of the critical part of HPT and HPC are within 5% errors compared to the finite element analysis results. The proposed method would significantly reduce computational workload and provide good reference for engine preliminary design. This method has significant practical value in engine component life prediction and management.

Original languageEnglish
Title of host publication2023 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2023, Proceedings - Volume I
EditorsSong Fu
PublisherSpringer Science and Business Media Deutschland GmbH
Pages291-299
Number of pages9
ISBN (Print)9789819739974
DOIs
StatePublished - 2024
Externally publishedYes
EventAsia-Pacific International Symposium on Aerospace Technology, APISAT 2023 - Lingshui, China
Duration: 16 Oct 202318 Oct 2023

Publication series

NameLecture Notes in Electrical Engineering
Volume1050 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceAsia-Pacific International Symposium on Aerospace Technology, APISAT 2023
Country/TerritoryChina
CityLingshui
Period16/10/2318/10/23

Keywords

  • Aeroengine
  • Preliminary design
  • State function
  • Stress

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