An efficient coupled-mode flutter analysis method for turbomachinery
Author:
Funder
National Major Science and Technology Project
Fundamental Research Funds for the Central Universities
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
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3. Velocity scaled aeroelastic testing of an unducted fan;Ducharme,1987
4. Coupling flutter of swept fan rotor blade with small aspect ratio;Wu;Hangkong Dongli Xuebao/J. Aerosp. Power,2014
5. Revisiting the one-shot method for modeling limit cycle oscillations: extension to two-degree-of-freedom systems;Li;Aerosp. Sci. Technol.,2017
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