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Quantification Parameter-Driven Uncertainty Analysis of Tip Clearance Deviation in Compressor Stability

  • Xi Yang
  • , Wuli Chu
  • , Tianyuan Ji
  • , Kaiye Liu
  • Northwestern Polytechnical University Xian

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

Abstract

Aero-engine advancements in thrust-to-weight ratio, reliability, intelligence, and multi-mode operation heighten sensitivity to compressor blade geometric deviations. Batch-produced engines show significant performance variations, with some failing stability margins due to machining deviations. This work employs NIPC-based uncertainty quantification with quantification parameter to rapidly assess Rotor 37 stability margins, validates parameter reliability, and analyzes tip clearance deviation impact mechanism.

Original languageEnglish
Title of host publicationMoving Integrated Product Development to Service Clouds in the Global Economy - Proceedings of the 21st ISPE Inc. International Conference on Concurrent Engineering, CE 2014
EditorsXuelin Lei
PublisherIOS Press BV
Pages288-295
Number of pages8
ISBN (Electronic)9781643686479
DOIs
StatePublished - 3 Mar 2026
Event16th International Conference of Mechanical and Aerospace Engineering, ICMAE 2025 - Rome, Italy
Duration: 15 Jul 202518 Jul 2025

Publication series

NameAdvances in Transdisciplinary Engineering
Volume87
ISSN (Print)2352-751X
ISSN (Electronic)2352-7528

Conference

Conference16th International Conference of Mechanical and Aerospace Engineering, ICMAE 2025
Country/TerritoryItaly
CityRome
Period15/07/2518/07/25

Keywords

  • Axial compressor
  • Quantification parameter
  • Stability
  • Tip clearance
  • Uncertainty quantification

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