Davide Antinolfi
Interlocking preload impact from creep effect on LPT blade vibration.
Rel. Christian Maria Firrone. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2022
Abstract: |
In this work the aeromechanical behavior of a rotoric stage of an LPT is described. The goal of this thesis is to understand how the dynamic response is affected by different boundary conditions. |
---|---|
Relators: | Christian Maria Firrone |
Academic year: | 2021/22 |
Publication type: | Electronic |
Number of Pages: | 58 |
Additional Information: | Tesi secretata. Fulltext non presente |
Subjects: | |
Corso di laurea: | Corso di laurea magistrale in Ingegneria Aerospaziale |
Classe di laurea: | New organization > Master science > LM-20 - AEROSPATIAL AND ASTRONAUTIC ENGINEERING |
Aziende collaboratrici: | GE AVIO S.R.L. |
URI: | http://webthesis.biblio.polito.it/id/eprint/22978 |
Modify record (reserved for operators) |