Novel parametric reduced order model for aeroengine blade dynamics-Reference-Cited by-同舟云学术

Novel parametric reduced order model for aeroengine blade dynamics

Published:2015-10 Issue: Volume:62-63 Page:235-253
ISSN:0888-3270
Container-title:Mechanical Systems and Signal Processing
language:en
Short-container-title:Mechanical Systems and Signal Processing

Author:

Yuan Jie,Allegri Giuliano,Scarpa Fabrizio^ORCID,Rajasekaran Ramesh,Patsias Sophoclis

Funder

Rolls-Royce plc

Composites University Technology Centre (UTC)

University of Bristol, UK

Strategic Investment in Low carbon Engine Technology (SILOET)

Rolls-Royce plc & the Technology Strategy Board (TSB)

China Scholarship Council

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference41 articles.

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3. The effects of detuning upon the forced vibrations of bladed disks;Ewins;J. Sound Vib.,1969

4. Confinement of vibration by structural irregularity;Hodges;J. Sound Vib.,1982

5. Vibration isolation from irregularity in a nearly periodic structure: theory and measurements;Hodges;J. Acoust. Soc. Am.,1983

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