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