PORTALE DELLA DIDATTICA

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  KEYWORD

Development of an integrated methodology to perform advanced aeromechanics analysis in a Low pressure turbine for aeronautical application

azienda 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