Analysis of experimental results of turbomachinery flutter using an asymptotic reduced order model

Detalhes bibliográficos
Autores: Rodríguez Blanco, Salvador|||0000-0002-1390-678X, Martel Escobar, Carlos|||0000-0001-7534-886X
Formato: artículo
Fecha de publicación:2021
País:España
Recursos:Universidad Politécnica de Madrid
Repositorio:Archivo Digital UPM
OAI Identifier:oai:oa.upm.es:87289
Acesso em linha:https://oa.upm.es/87289/
Access Level:acceso abierto
Palavra-chave:Asymptotics
Blade vibrations
Degrees of Freedom (Mechanics)
Design
Elastic Oscillations
Flutter
Flutter (Aerodynamics)
Friction
Integration time
Mass/spring systems
Mechanisms
Mistuned
Mistuning
Reduced order model
Reduced order modelling
Reduced-order model
Slip
Turbomachine Blades
Turbomachinery
vibration
Vibration amplitude
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