This paper presents an investigation of the influence of a nonconsistent approach in terms of mesh movement and mesh sensitivity calculationin a discrete adjoint-based optimization. Some mesh movement methods are more robust or of higher quality, whereas others can be more efficient for calculating mesh sensitivity. It is found that a nonconsistent approach gives comparable results when compared to a consistent approach. Therefore, an appropriate combination of nonconsistent approaches can be achieved for efficient adjoint optimization. This paper investigates and compares various consistent and nonconsistent combinations by using linear elasticity, Delaunay graph mapping, and radial basis function mesh movement methods. An investigation is...
A robust workflow for shape optimisation of internal and external flows with application to automoti...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
A grid movement algorithm based on the linear elasticity method with multiple increments is presente...
Aerodynamic optimisation using gradient-based methods has found a wide range of academic application...
A method based on the Delaunay graph mapping mesh movement is proposed to efficiently compute mesh s...
The purpose of this research is to use the surface sensitivity to aid the design and placement of fl...
In the present talk, the strategies to apply the sensitivity analysis method to aerodynamic shape op...
In the present talk, the strategies to apply the sensitivity analysis method to aerodynamic shape op...
This paper presents a new framework for Aerodynamic Shape Optimization (ASO) implemented inside the ...
PhDAdjoint based optimisation has until now demonstrated a great promise for optimisation in aerody...
A grid movement algorithm based on the linear elasticity method with multiple increments is presente...
An overview of twenty years of adjoint-based aerodynamic design research at NASA Langley Research Ce...
A continuous adjoint approach for obtaining sensitivity derivatives on unstructured grids is develop...
L’adaptation de maillage est un outil puissant pour l’obtention de simulations aérodynamiques précis...
Aerodynamic design optimization has been an important area of research for many years. Although some...
A robust workflow for shape optimisation of internal and external flows with application to automoti...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
A grid movement algorithm based on the linear elasticity method with multiple increments is presente...
Aerodynamic optimisation using gradient-based methods has found a wide range of academic application...
A method based on the Delaunay graph mapping mesh movement is proposed to efficiently compute mesh s...
The purpose of this research is to use the surface sensitivity to aid the design and placement of fl...
In the present talk, the strategies to apply the sensitivity analysis method to aerodynamic shape op...
In the present talk, the strategies to apply the sensitivity analysis method to aerodynamic shape op...
This paper presents a new framework for Aerodynamic Shape Optimization (ASO) implemented inside the ...
PhDAdjoint based optimisation has until now demonstrated a great promise for optimisation in aerody...
A grid movement algorithm based on the linear elasticity method with multiple increments is presente...
An overview of twenty years of adjoint-based aerodynamic design research at NASA Langley Research Ce...
A continuous adjoint approach for obtaining sensitivity derivatives on unstructured grids is develop...
L’adaptation de maillage est un outil puissant pour l’obtention de simulations aérodynamiques précis...
Aerodynamic design optimization has been an important area of research for many years. Although some...
A robust workflow for shape optimisation of internal and external flows with application to automoti...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
A grid movement algorithm based on the linear elasticity method with multiple increments is presente...