Interlocking preload impact from creep effect on LPT blade vibration

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

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