In the domain of fluid dynamics, the problem of shape optimization is relevant because is essential to increase lift and reduce drag forces on a body immersed in a fluid. The current state of the art in this aspect consists of two variants: (1) evolution from an initial guess, using optimization to achieve a very specific effect, (2) creation and genetic breeding of random individuals. These approaches achieve optimal shapes and evidence of response under parameter variation. Their disadvantages are the need of an approximated solution and / or the trial - and - error generation of individuals. In response to this situation, this manuscript presents a method which uses Fluid Mechanics indicators (e.g. streamline curvature, pressure differen...
Two constrained shape optimization problems relevant to aerodynamics are solved by genetic programmi...
An optimization procedure for the shape design of morphing aircraft is presented. The process is cou...
An optimization procedure for the shape design of morphing aircraft is presented. The process is cou...
In the domain of fluid dynamics, the problem of shape optimization is relevant because is essential ...
En el dominio de mecánica de fluidos, el problema de optimización de forma es relevante porqu...
The evaluation of fluid dynamic properties of various different structures is a computationally very...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
This study developed a framework for the shape optimization of aerodynamics profiles using computati...
Wing shape is an important factor affecting the aerodynamic performance of wings of monocopters and ...
This is the author accepted manuscript.Optimisation of designs using Computational Fluid Dynamics (C...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
Two constrained shape optimization problems relevant to aerodynamics are solved by genetic programmi...
An optimization procedure for the shape design of morphing aircraft is presented. The process is cou...
An optimization procedure for the shape design of morphing aircraft is presented. The process is cou...
In the domain of fluid dynamics, the problem of shape optimization is relevant because is essential ...
En el dominio de mecánica de fluidos, el problema de optimización de forma es relevante porqu...
The evaluation of fluid dynamic properties of various different structures is a computationally very...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
This study developed a framework for the shape optimization of aerodynamics profiles using computati...
Wing shape is an important factor affecting the aerodynamic performance of wings of monocopters and ...
This is the author accepted manuscript.Optimisation of designs using Computational Fluid Dynamics (C...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
Two constrained shape optimization problems relevant to aerodynamics are solved by genetic programmi...
An optimization procedure for the shape design of morphing aircraft is presented. The process is cou...
An optimization procedure for the shape design of morphing aircraft is presented. The process is cou...