Add to ORKGThe combination of the optimization software, modeFRONTIER and the commercial CFD software is used to optimize the aerodynamic functions of the airfoil, NACA0012. The N-S equations are adopted for calculating the airfoil aerodynamic properties (Cl, Cd and etc). Two kinds of optimization algorithm, the Multi-Object Genetic Algorithm (MOGA) and the Multi-Object Simulated Annealing (MOSA), are used in the optimization process respectively. The optimized airfoils show remarkable improvement of its aerodynamic functions (The ratio of lift to drag increases up to 282%) relative to its original one.EI0198-1022
This thesis presents a process to optimize a cambered airfoil with the MATLAB genetic algorithm (GA)...
Μη διαθέσιμη περίληψηNot available summarizationΠαρουσιάστηκε στο: 7th National Congress on Mechanic
There are different types of airfoil used in many applications such as energy production, aerospace,...
The method of optimization algorithms is one of the most important parameters which will strongly in...
This paper demonstrates the big influence of the control of the mesh quality in the final solution o...
AbstractComputational fluid dynamics (CFD) is one of the computer-based solution methods which is mo...
A multi-objective and multipoint optimization problem is presented dealing with a multi-element airf...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
In the modern engineering design cycle the use of computational tools becomes a neces- sity. The com...
This paper introduces a new version of the multiobjective Alliance Algorithm (MOAA) applied to the o...
Aerodynamic optimization is a very actual problem in aircraft design and airfoils are basic two-dime...
The Prediction of aerodynamic characteristics and shape optimization of airfoil under the ground eff...
This work focuses on an investigation of multi-modality in typical aerodynamic shape optimization pr...
Evolutionary algorithms (EAs) have been used to tackle non-linear multiobjective optimisation (MOO) ...
Abstract : The scheme of algorithm is decisively influence the result of aerodynamics shape optimiza...
This thesis presents a process to optimize a cambered airfoil with the MATLAB genetic algorithm (GA)...
Μη διαθέσιμη περίληψηNot available summarizationΠαρουσιάστηκε στο: 7th National Congress on Mechanic
There are different types of airfoil used in many applications such as energy production, aerospace,...
The method of optimization algorithms is one of the most important parameters which will strongly in...
This paper demonstrates the big influence of the control of the mesh quality in the final solution o...
AbstractComputational fluid dynamics (CFD) is one of the computer-based solution methods which is mo...
A multi-objective and multipoint optimization problem is presented dealing with a multi-element airf...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
In the modern engineering design cycle the use of computational tools becomes a neces- sity. The com...
This paper introduces a new version of the multiobjective Alliance Algorithm (MOAA) applied to the o...
Aerodynamic optimization is a very actual problem in aircraft design and airfoils are basic two-dime...
The Prediction of aerodynamic characteristics and shape optimization of airfoil under the ground eff...
This work focuses on an investigation of multi-modality in typical aerodynamic shape optimization pr...
Evolutionary algorithms (EAs) have been used to tackle non-linear multiobjective optimisation (MOO) ...
Abstract : The scheme of algorithm is decisively influence the result of aerodynamics shape optimiza...
This thesis presents a process to optimize a cambered airfoil with the MATLAB genetic algorithm (GA)...
Μη διαθέσιμη περίληψηNot available summarizationΠαρουσιάστηκε στο: 7th National Congress on Mechanic
There are different types of airfoil used in many applications such as energy production, aerospace,...