| KEYWORD |
11 - LAQ AerMec per componenti di turbine e compressori
Methodology development for advanced torsional dynamics analysis in aeronautical engine
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