An effective method is developed for efficient calculations of the sensitivity of the maximum forced response levels for mistuned bladed disks with respect to blade frequency mistuning. The expressions for 1st and 2nd order sensitivity coefficients are derived in an analytical form which provides high accuracy and computational efficiency. Then, the optimization methods are used for searching the best and worst mistuning patterns of bladed disks. Two major types of the mistuning optimization problems are considered: (i) a continuous optimization problem when the blade mistuning can take any values from a prescribed range and (ii) a combinatorial optimization problem, when the set of mistuned blades is given and the optimization can be achie...
In this paper a new approach to the mistune effects evaluation on turbomachine is presented that can...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...
ABSTRACT This paper focuses on the determination and study of the maximum amplification of the stead...
A method for searching For the worst frequency mistuning patterns (providing the highest response le...
Small deviations between turbine blades exist due to manufacturing tolerances or material inhomogene...
The newly revealed phenomenon of reduction of forced response levels in a mistuned bladed disk to le...
Mistuning affects forced response of bladed disks drastically; therefore, its identification plays a...
The problem of determining the maximum forced response vibration amplification that can be produced ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76794/1/AIAA-2005-2027-568.pd
The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently i...
This paper presents a test method to measure vibration characteristics of mistuned bladed disk syste...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76918/1/AIAA-2003-1544-512.pd
This paper presents a new approach to evaluating the mistuning effects on turbomachinery blades that...
In this paper a new approach to the mistune effects evaluation on turbomachine is presented that can...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...
ABSTRACT This paper focuses on the determination and study of the maximum amplification of the stead...
A method for searching For the worst frequency mistuning patterns (providing the highest response le...
Small deviations between turbine blades exist due to manufacturing tolerances or material inhomogene...
The newly revealed phenomenon of reduction of forced response levels in a mistuned bladed disk to le...
Mistuning affects forced response of bladed disks drastically; therefore, its identification plays a...
The problem of determining the maximum forced response vibration amplification that can be produced ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76794/1/AIAA-2005-2027-568.pd
The effect of small mistuning in the forced response of a bladed disk is analyzed using a recently i...
This paper presents a test method to measure vibration characteristics of mistuned bladed disk syste...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76918/1/AIAA-2003-1544-512.pd
This paper presents a new approach to evaluating the mistuning effects on turbomachinery blades that...
In this paper a new approach to the mistune effects evaluation on turbomachine is presented that can...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...