A numerical approach for the treatment of optimal shape problems governed by the Euler equations is discussed. Focus is on flows with embedded shocks. A very simple problem is considered: the design of a quasi-one-dimensional Laval nozzle. A cost function and a set of Lagrange multipliers are introduced to achieve the minimum. The nature of the resulting costate equations is discussed. A theoretical difficulty that arises for cases with embedded shocks is pointed out and solved. Finally, some results are given to illustrate the effectiveness of the method
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
This work describes the implementation of optimization techniques based on control theory for comple...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...
Optimal aerodynamic shape design aims to find the minimum of a functional that describes an aerodyna...
We exploit a novel idea for the optimization of flows governed by the Euler equations. The algorithm...
We consider a classical aerodynamic shape optimization problem subject to the compressible Euler flo...
An adjoint system of the Euler equations of gas dynamics is derived in order to solve aerodynamic sh...
In this paper, the exact discrete adjoint of an unstructured finite-volume formulation of the Euler ...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
In this paper the exact discrete adjoint of a finite volume formulation on unstructured meshes for t...
Abstract-Recently, shape design has been acquiring increasing relevance within the aeronautical comm...
Gradient-based aerodynamic shape optimization, based on Computational Fluid Dynamics analysis of the...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...
This paper studies the effect of design variables vector on automatic aerodynamic shape optimization...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
This work describes the implementation of optimization techniques based on control theory for comple...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...
Optimal aerodynamic shape design aims to find the minimum of a functional that describes an aerodyna...
We exploit a novel idea for the optimization of flows governed by the Euler equations. The algorithm...
We consider a classical aerodynamic shape optimization problem subject to the compressible Euler flo...
An adjoint system of the Euler equations of gas dynamics is derived in order to solve aerodynamic sh...
In this paper, the exact discrete adjoint of an unstructured finite-volume formulation of the Euler ...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
In this paper the exact discrete adjoint of a finite volume formulation on unstructured meshes for t...
Abstract-Recently, shape design has been acquiring increasing relevance within the aeronautical comm...
Gradient-based aerodynamic shape optimization, based on Computational Fluid Dynamics analysis of the...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...
This paper studies the effect of design variables vector on automatic aerodynamic shape optimization...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
This work describes the implementation of optimization techniques based on control theory for comple...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...