In this paper, a pre-existing reduction technique suitable for the analysis of mistuned bladed disk dynamics, the Component Mistuning Model technique (CMM), originally developed exclusively for the use of blade frequency mistuning pattern, is improved in order to allow for the introduction of a sector frequency mistuning pattern. If either mistuning is not confined to the blades (i.e. blades-to-disk interface mistuning), or the blades cannot be removed from the bladed disk (i.e. integral bladed disks), sector mistuning rather than blade mistuning is a more suitable choice to perturb the tuned system. The new version of the original technique is referred as CMM Upgrade (CMMU). After a theory review of the original technique, the modification...
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76847/1/AIAA-41214-408.pd
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
A new method for the dynamic analysis of mistuned bladed disks is presented. The method is based on ...
Nominally, a bladed disk assembly (single stage of a turbomachinery rotor) is a rotationally periodi...
The aim of this paper is to present a strategy for the prediction of the dynamic response of mistune...
The unavoidable existence of small differences between nominally identical sectors of bladed disks, ...
An efficient model order reduction technique for forced vibration analysis of a mistuned bladed disk...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76212/1/AIAA-2003-1545-961.pd
p. 1938-1950 A reduced-order model formulation is presented for examining the forced response of tun...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76499/1/AIAA-1994-1640-708.pd
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76847/1/AIAA-41214-408.pd
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
A new method for the dynamic analysis of mistuned bladed disks is presented. The method is based on ...
Nominally, a bladed disk assembly (single stage of a turbomachinery rotor) is a rotationally periodi...
The aim of this paper is to present a strategy for the prediction of the dynamic response of mistune...
The unavoidable existence of small differences between nominally identical sectors of bladed disks, ...
An efficient model order reduction technique for forced vibration analysis of a mistuned bladed disk...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76212/1/AIAA-2003-1545-961.pd
p. 1938-1950 A reduced-order model formulation is presented for examining the forced response of tun...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
A new reduced order modeling technique for nonlinear vibration analysis of mistuned bladed disks wit...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76499/1/AIAA-1994-1640-708.pd
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76847/1/AIAA-41214-408.pd
The effect of random blade mistuning on the dynamics of bladed disks is investigated. A reduced-orde...