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11 - LAQ AerMec per componenti di turbine e compressori

Dynamics of bladed disks in turboengines with friction contacts

keywords FRICTION, DYNAMIC, TURBINE

Reference persons TERESA MARIA BERRUTI

Research Groups 11 - LAQ AerMec per componenti di turbine e compressori

Thesis type MODELLISTICA-NUMERICA

Description Dynamic forced response calculation of bladed disk in turboengines with friction joints. An experimental Friction model will be used in the calculation

Required skills It would be appreciated a basic knowledge of the FEM software Ansys and of the Matlab software


Deadline 30/07/2018      PROPONI LA TUA CANDIDATURA




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