Adaptive perturbation scheme for the analysis of mistuned bladed disks

Chung Chih Lin, Marc Mignolet

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this paper, a novel perturbation technique is introduced for the determination of the forced vibration response of mistuned bladed disks. The proposed technique is adaptive in the sense that the level of approximation can be varied at will to accommodate any specificities of the tuned system and/or of the existing mistuning. This versatility of the proposed approach not only guarantees the reliability of the computed response but also leads to an excellent compromise between accuracy and computational effort. Numerical results are presented that demonstrate both the reliability of the computed response and the computational saving obtained by relying on the suggested perturbation technique as opposed to a straightforward steady state analysis.

Original languageEnglish (US)
Title of host publicationAmerican Society of Mechanical Engineers (Paper)
Editors Anon
PublisherASME
Publication statusPublished - 1995
EventProceedings of the International Gas Turbine and Aeroengine Congress and Exposition - Houston, TX, USA
Duration: Jun 5 1995Jun 8 1995

Other

OtherProceedings of the International Gas Turbine and Aeroengine Congress and Exposition
CityHouston, TX, USA
Period6/5/956/8/95

    Fingerprint

ASJC Scopus subject areas

  • Mechanical Engineering

Cite this

Lin, C. C., & Mignolet, M. (1995). Adaptive perturbation scheme for the analysis of mistuned bladed disks. In Anon (Ed.), American Society of Mechanical Engineers (Paper) ASME.