Bladed disks are components which dynamic behaviour are very sensitive to mistuning induced by the manufacturing process which makes blades differ from one another. This sensitivity increases in general the vibrations. The objective of this research is to propose new methods for optimizing design in vibration of bladed disks with respect to mistuning. Optimization is done for the forced response while keeping a sufficient aeroelastic stability margin. In this context, detuning by modifying geometrically the blades’ shapes is used. To reduce numerical computational costs, a new reduction method for geometrically detuned bladed disks is developed and validate. Uncertainties modeling including mistuning is done with a non-parametric probabilis...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76928/1/AIAA-2004-1686-437.pd
An effective method is developed for efficient calculations of the sensitivity of the maximum forced...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...
Bladed disks are components which dynamic behaviour are very sensitive to mistuning induced by the m...
International audienceIn the context of turbomachinery design, a small variation in the blade charac...
The research work reported in this dissertation aims to provide computational methodologies and to f...
The intentional mistuning, also called detuning has been identified as an efficient technological wa...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
International audienceA new method for vibration analysis of mistuned bladed disks is presented. The...
International audienceThe vibrational behavior of bladed-disks is known to be particularly complex i...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Bladed disks are used in various important engineering applications, such as fans, impeller pumps, w...
Efficient, novel design and analysis methods are presented for improving the structural performance ...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Nominally, a bladed disk assembly (single stage of a turbomachinery rotor) is a rotationally periodi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76928/1/AIAA-2004-1686-437.pd
An effective method is developed for efficient calculations of the sensitivity of the maximum forced...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...
Bladed disks are components which dynamic behaviour are very sensitive to mistuning induced by the m...
International audienceIn the context of turbomachinery design, a small variation in the blade charac...
The research work reported in this dissertation aims to provide computational methodologies and to f...
The intentional mistuning, also called detuning has been identified as an efficient technological wa...
Bladed disks are used in many important engineering applications, including turbine engine rotors. T...
International audienceA new method for vibration analysis of mistuned bladed disks is presented. The...
International audienceThe vibrational behavior of bladed-disks is known to be particularly complex i...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Bladed disks are used in various important engineering applications, such as fans, impeller pumps, w...
Efficient, novel design and analysis methods are presented for improving the structural performance ...
International audienceOne major industrial challenge is to consider the detuning as a technological ...
Nominally, a bladed disk assembly (single stage of a turbomachinery rotor) is a rotationally periodi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76928/1/AIAA-2004-1686-437.pd
An effective method is developed for efficient calculations of the sensitivity of the maximum forced...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...