KEYWORD |
11 - LAQ AerMec per componenti di turbine e compressori
Theses in external company
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