Based on Bezier curve, experimental design theory, and response surface method, the optimization design method for turbine blades is established. The turbine of turbodrill tested on the bench is taken for an example, and the numerical simulation model is established using third-order Bezier curve fitting blade surfaces. The model is then verified by test experiment data of the turbine bench and proven to be reliable. The blade structure parameters are defined as independent variables, and the maximum efficiency is defined as the objective function. Based on the simulation results by the computational fluid dynamics, first the significant impacts on the blade profile parameters are filtered out by seven times in single-factor sensitive analy...
Abstract: An improved aerodynamic optimization technique for two-dimensional wind turbine airfoils i...
AbstractAn optimization procedure has been developed for the efficient design of turbine blade airfo...
A method is presented to perform aerodynamic design optimization of turbomachinery blades. The metho...
AbstractIn order to improve turbine internal efficiency and lower manufacturing cost, a new highly l...
An adjoint-response surface method is developed to give global representation of cost function in a ...
A multidisciplinary optimization procedure, with the integration of aerodynamic and heat transfer cr...
Turbomachinery blade profiles in use today were all derived out of conventional methods. For example...
Turbodrill is a type of hydraulic axial turbomachinery which has a multistage blade consisting of st...
Utilization of hydro-power as renewable energy source is of prime importance in the world now. Hydro...
This paper presents a design method for two-dimensional transonic turbine blades. It couples a Navie...
Compressor and turbine blade design involves thermodynamical, aerodynamical and mechanical aspects, ...
The main goal in jet engine design is to achieve light, compact and highly efficient systems while r...
The present study aims to numerically determine the geometric proportions that maximize the performa...
The new method and algorithm of three-dimensional turbine guide blade rim optimization were proposed...
In a conventional design and manufacturing process, turbine blades are modeled based on reverse engi...
Abstract: An improved aerodynamic optimization technique for two-dimensional wind turbine airfoils i...
AbstractAn optimization procedure has been developed for the efficient design of turbine blade airfo...
A method is presented to perform aerodynamic design optimization of turbomachinery blades. The metho...
AbstractIn order to improve turbine internal efficiency and lower manufacturing cost, a new highly l...
An adjoint-response surface method is developed to give global representation of cost function in a ...
A multidisciplinary optimization procedure, with the integration of aerodynamic and heat transfer cr...
Turbomachinery blade profiles in use today were all derived out of conventional methods. For example...
Turbodrill is a type of hydraulic axial turbomachinery which has a multistage blade consisting of st...
Utilization of hydro-power as renewable energy source is of prime importance in the world now. Hydro...
This paper presents a design method for two-dimensional transonic turbine blades. It couples a Navie...
Compressor and turbine blade design involves thermodynamical, aerodynamical and mechanical aspects, ...
The main goal in jet engine design is to achieve light, compact and highly efficient systems while r...
The present study aims to numerically determine the geometric proportions that maximize the performa...
The new method and algorithm of three-dimensional turbine guide blade rim optimization were proposed...
In a conventional design and manufacturing process, turbine blades are modeled based on reverse engi...
Abstract: An improved aerodynamic optimization technique for two-dimensional wind turbine airfoils i...
AbstractAn optimization procedure has been developed for the efficient design of turbine blade airfo...
A method is presented to perform aerodynamic design optimization of turbomachinery blades. The metho...