The effect of mistuning on the vibration of bladed disks has been extensively studied in the past 30 years. Most of these analysis typically cover the case of small variations of the elastic characteristics (mass and stiffness) of the blades. In this work we study the not so common case of the forced response of a stable rotor with damping mistuning. The Asymptotic Mistuning Model (AMM) is used to analyze this problem. The AMM methodology provides a simplified model that describes the effect of blade to blade damping variation, and gives precise information on the underlying mechanisms involved in the action of damping mistuning
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
One of the most important problems that plague turbomachinery rotors is the existence of rogue blade...
The effect of mistuning on the vibration of bladed disks has been extensively studied in the past 30...
Mistuning can dangerously increase the vibration amplitude of the forced response of a turbomachiner...
ABSTRACT The problem of determining the maximum forced response vibration amplification that can be ...
The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently i...
Mistuning can produce a considerable increase of the vibratory forced response of the blades compare...
The newly revealed phenomenon of reduction of forced response levels in a mistuned bladed disk to le...
Intentional mistuning is a common procedure to decrease the uncontrolled vibration amplification eff...
The problem of determining the maximum forced response vibration amplification that can be produced ...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Mistuning of bladed disks in turbo-machinery is practically unavoidable. Small mistuning may result ...
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...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
One of the most important problems that plague turbomachinery rotors is the existence of rogue blade...
The effect of mistuning on the vibration of bladed disks has been extensively studied in the past 30...
Mistuning can dangerously increase the vibration amplitude of the forced response of a turbomachiner...
ABSTRACT The problem of determining the maximum forced response vibration amplification that can be ...
The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently i...
Mistuning can produce a considerable increase of the vibratory forced response of the blades compare...
The newly revealed phenomenon of reduction of forced response levels in a mistuned bladed disk to le...
Intentional mistuning is a common procedure to decrease the uncontrolled vibration amplification eff...
The problem of determining the maximum forced response vibration amplification that can be produced ...
The unavoidable small blade-to-blade variations in a turbomachinery bladed disk are know as "mistuni...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Mistuning of bladed disks in turbo-machinery is practically unavoidable. Small mistuning may result ...
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...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
One of the most important problems that plague turbomachinery rotors is the existence of rogue blade...