Fatigue failure in blades resulting from alternating loads is a primary cause of aircraft engine
failure. In this study, the dynamic and fatigue performance of a compressor blade, which is …

The vibration stress caused by resonance is the main cause of failure in aircraft engine
blades. The study investigated the vibration stress of a single-stage fan blade influenced by …

Gas turbine engine components are subject to both low-cycle fatigue (LCF) and high-cycle
fatigue (HCF) loads. To improve engine reliability, durability and maintenance, it is …

In this paper, the vibrational analysis of the turbine blade and the effect of pressure on the
rotor surface in the fluid–structure interaction are investigated. Due to the complex and …

Gas turbines are very important because they can be used in several areas, such as
aeronautics and electric power generation systems. The operation of a gas turbine can be …

In this paper we discuss different possibilities of using partially ordered sets of grids in
multigrid algorithms. Because, for a classical sequence of regular grids the number of …

Abstract Analysis of the aerodynamic, thermal and aeroelasticity (including vibration)
processes in gas turbine stage is principal for a design and creating turbines and jet engine …

Turbine stages are exposed to a variety of excitation sources in the power industry. The
resulting forced vibration excitation of the blades may occur near a blade's natural …

Газовые турбины являются неотъемлемой частью газотурбинных двигателей (ГТД),
позволяющей преобразовать энтальпию продуктов сгорания в механическую работу на …

Università degli Studi di Padova Page 1 Università degli Studi di Padova Dipartimento di
Ingegneria Industriale Corso di Laurea Magistrale in Ingegneria Meccanica Tesi di Laurea …