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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

azienda Thesis in external company    


keywords BLADED DISK DYNAMICS, TURBINE

Reference persons DANIELE BOTTO

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

Thesis type MASTER THESIS

Description 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.

Required skills MS engineering students (energy, aerospace, mechanical or equivalent).
Bonus: Finite Element Analysis and vibration mechanics.

Notes Duration: 8 months
Location of the internship: GE-AVIO


Deadline 09/03/2020      PROPONI LA TUA CANDIDATURA




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