A study of mode localization in mistuned bladed disks is performed using transfer matrices. The transfer matrix approach yields the free response of a general, mono-coupled, perfectly cyclic assembly in closed form. A mistuned structure is represented by random transfer matrices, and the expansion of these matrices in terms of the small mistuning parameter leads to the definition of a measure of sensitivity to mistuning. An approximation of the localization factor, the spatially averaged rate of exponential attenuation per blade-disk sector, is obtained through perturbation techniques in the limits of high and low sensitivity. The methodology is applied to a common model of a bladed disk and the results verified by Monte Carlo simulations. ...
International audienceA new method for vibration analysis of mistuned bladed disks is presented. The...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76847/1/AIAA-41214-408.pd
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
This thesis investigates techniques for predicting when small blade-to-blade dissimilarity can lead ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76499/1/AIAA-1994-1640-708.pd
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...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76918/1/AIAA-2003-1544-512.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76142/1/AIAA-1991-1218-735.pd
An investigation of the effects of small mistuning on the aeroelastic modes of bladed disk assemblie...
The adverse effects of small, random structural irregularities among the blades, called mistuning, c...
Nominally, a bladed disk assembly (single stage of a turbomachinery rotor) is a rotationally periodi...
peer reviewedAlthough a bladed disk is typically designed to have identical blades, manufacturing to...
The adverse effects of small, random structural irregularities among the blades, called mistuning, c...
The research work reported in this dissertation aims to provide computational methodologies and to f...
International audienceA new method for vibration analysis of mistuned bladed disks is presented. The...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76847/1/AIAA-41214-408.pd
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...
This thesis investigates techniques for predicting when small blade-to-blade dissimilarity can lead ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76499/1/AIAA-1994-1640-708.pd
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...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76918/1/AIAA-2003-1544-512.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76142/1/AIAA-1991-1218-735.pd
An investigation of the effects of small mistuning on the aeroelastic modes of bladed disk assemblie...
The adverse effects of small, random structural irregularities among the blades, called mistuning, c...
Nominally, a bladed disk assembly (single stage of a turbomachinery rotor) is a rotationally periodi...
peer reviewedAlthough a bladed disk is typically designed to have identical blades, manufacturing to...
The adverse effects of small, random structural irregularities among the blades, called mistuning, c...
The research work reported in this dissertation aims to provide computational methodologies and to f...
International audienceA new method for vibration analysis of mistuned bladed disks is presented. The...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76847/1/AIAA-41214-408.pd
Bladed disks are critical structural components in jet engines and other turbomachinery. The nominal...