Investigation on aeroelastic characteristics of mistuned low-speed axial compressor rotor: Numerical methodology and optimization-Reference-Cited by-同舟云学术

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Investigation on aeroelastic characteristics of mistuned low-speed axial compressor rotor: Numerical methodology and optimization

Published:2023-12 Issue: Volume:143 Page:108735
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Fan Chengwei,Adjei Richard Amankwa,Ye Zhouteng^ORCID,Cui Jiahuan^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Flutter and resonant vibration characteristics of engine blades;Srinivasan;Int. Gas Turbine Aeroengine Congr. Exhib.,1997

2. Numerical simulations of flutter mechanism for high-speed wide-chord transonic fan;Dong;Aerosp. Sci. Technol.,2020

3. Flutter and Forced Response of Turbomachinery with Frequency Mistuning and Aerodynamic Asymmetry;Miyakozawa,2008

4. The maximum factor by which forced vibration of blades can increase due to mistuning;Whitehead;Int. Gas Turbine Aeroengine Congr. Exhib.,1996

5. Maximum amplification of blade response due to mistuning: localization and mode shapes aspects of the worst disks;Rivas-Guerra,2002

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