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Modal analysis of the nozzle guide vane in low pressure turbine system of aircraft engine

  • Silesian University of Technology
  • AvioPolska Sp. z o.o

Research output: Contribution to journal › Conference article › peer-review

2 Citations (Scopus)

Abstract

The aim of the article is to present modal analysis of nozzle guide vane in low pressure turbine system of aircraft engine. Comparison of results obtained by means of finite element analysis with results of experimental one in terms of frequencies and modal forms are presented. Additionally, the article presents consistent results which will be used in further analyses and researches related to the optimization of dynamic characteristics with application of artificial intelligence.

Original languageEnglish
Article number012049
JournalIOP Conference Series: Materials Science and Engineering
Volume1037
Issue number1
DOIs
Publication statusPublished - 11 Feb 2021
Event24th Innovative Manufacturing Engineering and Energy International Conference, IManEE 2020 - Athens, Greece
Duration: 14 Dec 2020 → 15 Dec 2020

ASJC Scopus subject areas

  • General Materials Science
  • General Engineering

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