The discrete adjoint of a reconstruction-based unstructured finite volume formulation for the Euler equations is derived and implemented. The matrix-vector products required to solve the adjoint equations are computed on-the-fly by means of an efficient two-pass assembly. The adjoint equations are solved with the same solution scheme adopted for the flow equations. The scheme is modified to efficiently account for the simultaneous solution of several adjoint equations. The implementation is demonstrated on wing and wing–body configurations
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76366/1/AIAA-1993-65-412.pd
A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstr...
The discrete adjoint of a reconstruction-based unstructured finite volume formulation for the Euler ...
textabstractThe discrete adjoint of a reconstruction-based unstructured finite volume formulation fo...
In this paper the exact discrete adjoint of a finite volume formulation on unstructured meshes for t...
In this paper, the exact discrete adjoint of an unstructured finite-volume formulation of the Euler ...
A methodology for aerodynamic shape optimization on two-dimensional unstructured grids using Euler e...
The complete discrete adjoint equations for an unstructured finite volume compressible Navier-Stokes...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...
A design optimization method based on three dimensional Euler equations is developed. A finite volum...
A systematic methodology for formulating, implementing, solving and verifying discrete adjoint of th...
This paper presents a number of algorithm developments for adjoint methods using the 'discrete' appr...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The gradie...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76366/1/AIAA-1993-65-412.pd
A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstr...
The discrete adjoint of a reconstruction-based unstructured finite volume formulation for the Euler ...
textabstractThe discrete adjoint of a reconstruction-based unstructured finite volume formulation fo...
In this paper the exact discrete adjoint of a finite volume formulation on unstructured meshes for t...
In this paper, the exact discrete adjoint of an unstructured finite-volume formulation of the Euler ...
A methodology for aerodynamic shape optimization on two-dimensional unstructured grids using Euler e...
The complete discrete adjoint equations for an unstructured finite volume compressible Navier-Stokes...
Aerospace industry is increasingly relying on advanced numerical flow simulation tools in the early ...
A design optimization method based on three dimensional Euler equations is developed. A finite volum...
A systematic methodology for formulating, implementing, solving and verifying discrete adjoint of th...
This paper presents a number of algorithm developments for adjoint methods using the 'discrete' appr...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.The gradie...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76366/1/AIAA-1993-65-412.pd
A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstr...