peer reviewedAlthough a bladed disk is typically designed to have identical blades, manufacturing tolerances, wear, and other causes may cause random deviations among the blades. The blade-to-blade discrepancies, denoted as mistuning, lead to vibratory responses mostly concentrated in small regions of the bladed-disk assembly, according to a phenomenon called localization. The resulting spatial confinement of the vibration energy causes the responses of some blades to become dangerously high and increases the amplitude of the bladed-disk assembly's overall response. The attendant increase in stresses can lead to premature high cycle fatigue (HCF) of the blades. In this study we investigate whether vibration localization in a perfectly symme...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
peer reviewedThe objective of this study is to carry out modal analysis of nonlinear periodic struct...
This article examines a lump mass model of a perfectly symmetric bladed disk assembly of five sector...
The objective of this study is to carry out modal analysis of nonlinear periodic structures using n...
Abstract: A simple model of blade interactions through an elastic disk is suggested in this paper. T...
This thesis investigates techniques for predicting when small blade-to-blade dissimilarity can lead ...
ABSTRACT The objective of this study is to carry out modal analysis of nonlinear periodic structures...
A study of mode localization in mistuned bladed disks is performed using transfer matrices. The tran...
Mistuning, small differences among sectors of bladed disks, is unavoidable because of manufacturing ...
Mistuning, small differences among sectors of bladed disks, is unavoidable because of manufacturing ...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Mistuning can produce a considerable increase of the vibratory forced response of the blades compare...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
peer reviewedThe objective of this study is to carry out modal analysis of nonlinear periodic struct...
This article examines a lump mass model of a perfectly symmetric bladed disk assembly of five sector...
The objective of this study is to carry out modal analysis of nonlinear periodic structures using n...
Abstract: A simple model of blade interactions through an elastic disk is suggested in this paper. T...
This thesis investigates techniques for predicting when small blade-to-blade dissimilarity can lead ...
ABSTRACT The objective of this study is to carry out modal analysis of nonlinear periodic structures...
A study of mode localization in mistuned bladed disks is performed using transfer matrices. The tran...
Mistuning, small differences among sectors of bladed disks, is unavoidable because of manufacturing ...
Mistuning, small differences among sectors of bladed disks, is unavoidable because of manufacturing ...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Mistuning can produce a considerable increase of the vibratory forced response of the blades compare...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...