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  KEYWORD

Methodology development for advanced torsional dynamics analysis in aeronautical engine

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 study a methodology to assess the torsional dynamic behavior of accessory drive trains of aeronautical engines, featuring highly non-linear transients in several different scenarios: engine start, engine relight ecc… The validation phase will consist in dealing with experimental data post-processing and model tuning, to improve the accuracy and robustness of the developed simulation methods.

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


Deadline 09/03/2019      PROPONI LA TUA CANDIDATURA