peer reviewedThe dynamic behavior of bladed disks in resonance crossing has been intensively investigated in the community of turbomachinery, addressing the attention to (1) the transient-type response that appear when the resonance is crossed with a finite sweep rate and (2) the localization of the vibration in the disk due to the blade mistuning. In real conditions, the two mentioned effects coexist and can interact in a complex manner. This paper investigates the problem by means of analytic solutions obtained through asymptotic expansions, as well as numerical simulations. The mechanical system is assumed as simple as possible: a 2-dof linear system defined through the three parameters: damping ratio , frequency mistuning , rotor accele...
Mistuning can dangerously increase the vibration amplitude of the forced response of a turbomachiner...
Small mistuning can cause large, catastrophic changes in blade vibrational response whereby the ampl...
This paper is focused on the analysis of effects of mistuning on the forced response of gas-turbine ...
peer reviewedThe dynamic behavior of bladed disks in resonance crossing has been intensively invest...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently i...
The problem of determining the maximum forced response vibration amplification that can be produced ...
ABSTRACT The problem of determining the maximum forced response vibration amplification that can be ...
This thesis investigates techniques for predicting when small blade-to-blade dissimilarity can lead ...
abstract: Mistuning is defined as the blade-to-blade variation of bladed disks caused by slight chan...
Mistuning can produce a considerable increase of the vibratory forced response of the blades compare...
The research work reported in this dissertation aims to provide computational methodologies and to f...
One of the most important problems that plague turbomachinery rotors is the existence of rogue blade...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
Mistuning can dangerously increase the vibration amplitude of the forced response of a turbomachiner...
Small mistuning can cause large, catastrophic changes in blade vibrational response whereby the ampl...
This paper is focused on the analysis of effects of mistuning on the forced response of gas-turbine ...
peer reviewedThe dynamic behavior of bladed disks in resonance crossing has been intensively invest...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently i...
The problem of determining the maximum forced response vibration amplification that can be produced ...
ABSTRACT The problem of determining the maximum forced response vibration amplification that can be ...
This thesis investigates techniques for predicting when small blade-to-blade dissimilarity can lead ...
abstract: Mistuning is defined as the blade-to-blade variation of bladed disks caused by slight chan...
Mistuning can produce a considerable increase of the vibratory forced response of the blades compare...
The research work reported in this dissertation aims to provide computational methodologies and to f...
One of the most important problems that plague turbomachinery rotors is the existence of rogue blade...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
Mistuning can dangerously increase the vibration amplitude of the forced response of a turbomachiner...
Small mistuning can cause large, catastrophic changes in blade vibrational response whereby the ampl...
This paper is focused on the analysis of effects of mistuning on the forced response of gas-turbine ...