In order to draw in and compass gas (most usually air) into the gas turbines, compressor section is designed. Then, the compressed air will be combined with fuel to generate heat and extract power. Blades of the compressor section of the gas turbine can be produced by machining operations. Machining operations of turbine blades by using 4 and 5 Axis CNC machine tools are always with complexities and challenges which can be analyzed and optimized. So, research works which can increase efficiency of blades production are always in attention of manufacturing companies.To optimize machining operations, finite element analysis of produced turbine blades is implemented by using the Abaqus software. So, stress, strain and deformation of blades in ...
An aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element Momentum ...
Abstract. The design of 2-D turbine blades using tar-get pressure considerations is described. It is...
There is evidence of a lack of knowledge in the design of the blade/disk attachment so that the stre...
In order to draw in and compass gas (most usually air) into the gas turbines, compressor section is ...
To simulate and analyze the real machined parts in virtual environments, virtual machining systems a...
A multidisciplinary optimization procedure, with the integration of aerodynamic and heat transfer cr...
AbstractThe gas turbine is the heart of all modern aircraft. The power derived from the gas turbine ...
MasterModern industrial axial compressor requires high performance for cost saving. The internal flo...
In this paper we present a fully automated procedure for turbine blade op- timisation. Optimisatio...
The blades have the effect of removing energy in the hot temperature, ruthless gas created through t...
This paper presents a description of the method and results of rotor blade shape optimization. The r...
In a conventional design and manufacturing process, turbine blades are modeled based on reverse engi...
To simulate and analyse the real machined parts in virtual environments, virtual machining systems a...
The article presents one of the possible methods for optimizing the blade shape of a Francis radial-...
In the gas turbine, the power is generated at higher temperature and large magnitude, the results of...
An aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element Momentum ...
Abstract. The design of 2-D turbine blades using tar-get pressure considerations is described. It is...
There is evidence of a lack of knowledge in the design of the blade/disk attachment so that the stre...
In order to draw in and compass gas (most usually air) into the gas turbines, compressor section is ...
To simulate and analyze the real machined parts in virtual environments, virtual machining systems a...
A multidisciplinary optimization procedure, with the integration of aerodynamic and heat transfer cr...
AbstractThe gas turbine is the heart of all modern aircraft. The power derived from the gas turbine ...
MasterModern industrial axial compressor requires high performance for cost saving. The internal flo...
In this paper we present a fully automated procedure for turbine blade op- timisation. Optimisatio...
The blades have the effect of removing energy in the hot temperature, ruthless gas created through t...
This paper presents a description of the method and results of rotor blade shape optimization. The r...
In a conventional design and manufacturing process, turbine blades are modeled based on reverse engi...
To simulate and analyse the real machined parts in virtual environments, virtual machining systems a...
The article presents one of the possible methods for optimizing the blade shape of a Francis radial-...
In the gas turbine, the power is generated at higher temperature and large magnitude, the results of...
An aerodynamic shape optimization methodology based on Genetic Algorithm and Blade Element Momentum ...
Abstract. The design of 2-D turbine blades using tar-get pressure considerations is described. It is...
There is evidence of a lack of knowledge in the design of the blade/disk attachment so that the stre...