Tabu genetic cat swarm optimization algorithm is proposed for optimization arrangement on mistuned blades. Furthermore, it is improved to be an innovative parallel algorithm based on Compute Unified Device Architecture (CUDA), whose performance is analyzed both in continuous and discrete solution space. The lumped parameter model and finite element model of the bladed-disk system are established for dynamics analysis and optimization verification. The complete mistuned parameter identification method and the improved mixed-interface prestressed substructure modal synthesis method are two other highlights. The results indicate that the algorithm in this paper has the advantages of low cost and high efficiency. The vibration localization and ...
The recent progresses in simulation technologies in several fields such as CFD, structures, thermal ...
The process of designing a wind turbine blade involves many disciplines and is of an iterative chara...
Abstract. The design of 2-D turbine blades using tar-get pressure considerations is described. It is...
This paper sets up a lumped parameter model of engine bladed disk system when considering the nonlin...
In this paper a new approach to the mistune effects evaluation on turbomachine is presented that can...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...
AbstractAn aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element M...
The coaxiality and unbalance are the two important indexes to evaluate the assembly quality of an ae...
An aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element Momentum ...
This paper describes an optimization method for the design of horizontal axis wind turbines using th...
Multi-stage disc rotor assembly is an important part of the aero-engine rotor manufacturing process....
This paper investigates the application of blade pitch angle controller to stabilize the frequency a...
An effective method is developed for efficient calculations of the sensitivity of the maximum forced...
LUY, Murat/0000-0002-2378-0009; Cam, Ertugrul/0000-0001-6491-9225WOS: 000384016100020Output powers o...
Designing the optimal shape of MW wind turbine blades is provided in a number of cases through evolu...
The recent progresses in simulation technologies in several fields such as CFD, structures, thermal ...
The process of designing a wind turbine blade involves many disciplines and is of an iterative chara...
Abstract. The design of 2-D turbine blades using tar-get pressure considerations is described. It is...
This paper sets up a lumped parameter model of engine bladed disk system when considering the nonlin...
In this paper a new approach to the mistune effects evaluation on turbomachine is presented that can...
This paper investigates methodologies for finding optimal or near-optimal blade arrangements in a bl...
AbstractAn aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element M...
The coaxiality and unbalance are the two important indexes to evaluate the assembly quality of an ae...
An aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element Momentum ...
This paper describes an optimization method for the design of horizontal axis wind turbines using th...
Multi-stage disc rotor assembly is an important part of the aero-engine rotor manufacturing process....
This paper investigates the application of blade pitch angle controller to stabilize the frequency a...
An effective method is developed for efficient calculations of the sensitivity of the maximum forced...
LUY, Murat/0000-0002-2378-0009; Cam, Ertugrul/0000-0001-6491-9225WOS: 000384016100020Output powers o...
Designing the optimal shape of MW wind turbine blades is provided in a number of cases through evolu...
The recent progresses in simulation technologies in several fields such as CFD, structures, thermal ...
The process of designing a wind turbine blade involves many disciplines and is of an iterative chara...
Abstract. The design of 2-D turbine blades using tar-get pressure considerations is described. It is...