<p>The truncation error estimation methodology using topologically inconsistent fine and coarse meshes was<br> presented. Estimated truncation error was weighted with an adjoint solution to obtain a robust output-based adaptation<br> sensor.<br> Re-meshing using Boxer and output-based sensor field was successfully applied to the simple cube test case showing<br> almost an order of magnitude cost function error reduction as compared to the uniformly refined grid.<br> More application examples are required including a more realistic turbulent cases e.g. turbine stator in order to investigate how useful is the methodology in practice.<br> The key challenge for viscous flows is related to the treatment of boundary layer when performing re-meshi...
A numerical procedure is presented which uses the truncation error injection methodology to efficien...
The aerospace research and industry sectors are relying increasingly on numerical simulations to gai...
We present adjoint-based techniques to estimate the error of a numerical flow solution with respect ...
The truncation error estimation methodology using topologically inconsistent fine and coarse meshes ...
Error quantification for industrial CFD requires a new paradigm in which a robust flow solver with e...
Mesh adaptation based on error estimation has become a key technique to improve th eaccuracy o fcom...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90641/1/AIAA-53965-537.pd
This article reviews recent work in output-based error estimation and mesh adaptation for Computatio...
<p>Output-based R-refinement and the Use of Geometric Multigrid for Truncation Error Estimation in C...
Nowadays, aerodynamic computational modeling is carried out on a daily basis in an industrial settin...
PhDThe adjoint method in computational fluid dynamics (CFD) made shape optimisation affordable. Howe...
This paper examines different approaches for driving mesh adaptation and provides theoretical develo...
As aerospace design programs rely more on computational fluid dynamics (CFD) in all phases of the en...
In 2011 a relatively new type of numerical scheme has been introduced: Active Flux schemes. In this ...
International audienceAdaptive methods have been widely used in aeronautics to improve the predictio...
A numerical procedure is presented which uses the truncation error injection methodology to efficien...
The aerospace research and industry sectors are relying increasingly on numerical simulations to gai...
We present adjoint-based techniques to estimate the error of a numerical flow solution with respect ...
The truncation error estimation methodology using topologically inconsistent fine and coarse meshes ...
Error quantification for industrial CFD requires a new paradigm in which a robust flow solver with e...
Mesh adaptation based on error estimation has become a key technique to improve th eaccuracy o fcom...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90641/1/AIAA-53965-537.pd
This article reviews recent work in output-based error estimation and mesh adaptation for Computatio...
<p>Output-based R-refinement and the Use of Geometric Multigrid for Truncation Error Estimation in C...
Nowadays, aerodynamic computational modeling is carried out on a daily basis in an industrial settin...
PhDThe adjoint method in computational fluid dynamics (CFD) made shape optimisation affordable. Howe...
This paper examines different approaches for driving mesh adaptation and provides theoretical develo...
As aerospace design programs rely more on computational fluid dynamics (CFD) in all phases of the en...
In 2011 a relatively new type of numerical scheme has been introduced: Active Flux schemes. In this ...
International audienceAdaptive methods have been widely used in aeronautics to improve the predictio...
A numerical procedure is presented which uses the truncation error injection methodology to efficien...
The aerospace research and industry sectors are relying increasingly on numerical simulations to gai...
We present adjoint-based techniques to estimate the error of a numerical flow solution with respect ...