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The paper deals with a simply supported cylindrical shell rotating about its longitudinal axis. The shell is modelled according to the thin shell theory and small deflection assumption. The equations of relative motion are derived considering the acceleration including the Coriolis component. The analysis is focused on the passive damping effect created by viscoelastic material. The complex eigenvalue problem is formulated and solved. The results show the influence of material damping property on the modal equivalent damping parameter for variations in the angular velocity of the shell. The relations between the modal damping parameter and velocity of rotation for different retardation time (loss factor) values are also presented.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
113--120
Opis fizyczny
Bibliogr. 6 poz.
Twórcy
autor
- Warsaw University of Technology Institute of Machine Design Fundamentals Narbutta 84, 02-524 Warszawa, Polska Phone 660-85-32
autor
- Warsaw University of Technology Institute of Machine Design Fundamentals Narbutta 84, 02-524 Warszawa, Polska Phone 660-85-32
autor
- Warsaw University of Technology Institute of Machine Design Fundamentals Narbutta 84, 02-524 Warszawa, Polska Phone 660-85-32
Bibliografia
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-c8138dd2-1616-4a3c-bd96-26f53c3ca326