| KEYWORD |
11 - LAQ AerMec per componenti di turbine e compressori
Development of an integrated methodology to perform advanced aeromechanics analysis in a Low pressure turbine for aeronautical application
Tesi esterna in azienda
Parole chiave BLADED DISK DYNAMICS, TURBINE
Riferimenti DANIELE BOTTO
Gruppi di ricerca 11 - LAQ AerMec per componenti di turbine e compressori
Tipo tesi MASTER THESIS
Descrizione This activity will consist in the development of a tool for assessing the aeromech behavior (linear and nonlinear) of a cyclic structure in a low pressure turbine. Specific test cases will be used to validate the tool.
Conoscenze richieste MS engineering students (energy, aerospace, mechanical or equivalent).
Bonus: Finite Element Analysis and vibration mechanics.
Note Duration: 8 months
Location of the internship: GE-AVIO
Scadenza validita proposta 09/03/2020
PROPONI LA TUA CANDIDATURA