Davide Antinolfi
Interlocking preload impact from creep effect on LPT blade vibration.
Rel. Christian Maria Firrone. Politecnico di Torino, Master of science program in Aerospace Engineering, 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
Academic year
Publication type
Number of Pages
Additional Information
Course of studies
Classe di laurea
Aziende collaboratrici
URI
 |
Modify record (reserved for operators) |
