Assessment of Error Estimation Methods with an Emphasis on Local Error in Applied Flows

The capabilities of a-posteriori discretisation error estimation methods is investigated with an emphasis on local flow variables in aerodynamic flows. Sets of meshes are generated for three different test cases that represent typical aerodynamic flow features. Simulations are carried out using the TAU-Code solver developed by the German Aerospace Center (DLR). Performance of the estimation methods to locate the error correctly is first judged by visual inspection. In addition, a quantitative error measurement is introduced to validate the accuracy of the magnitude estimation. Ultimately, the study aims to lay a foundation for error estimation in complex geometries and provides a basis for grid requirements and local grid refinement.

Publication Details

Journal
Deutsche Gesellschaft für Luft- und Raumfahrt
Published
2024-11-13
DOI
https://doi.org/10.25967/630051
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
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article

Assessment of Error Estimation Methods with an Emphasis on Local Error in Applied Flows

Deutsche Gesellschaft für Luft- und Raumfahrt
Computational Fluid Dynamics and Aerodynamics
article

Assessment of Error Estimation Methods with an Emphasis on Local Error in Applied Flows

article en

Abstract

The capabilities of a-posteriori discretisation error estimation methods is investigated with an emphasis on local flow variables in aerodynamic flows. Sets of meshes are generated for three different test cases that represent typical aerodynamic flow features. Simulations are carried out using the TAU-Code solver developed by the German Aerospace Center (DLR). Performance of the estimation methods to locate the error correctly is first judged by visual inspection. In addition, a quantitative error measurement is introduced to validate the accuracy of the magnitude estimation. Ultimately, the study aims to lay a foundation for error estimation in complex geometries and provides a basis for grid requirements and local grid refinement.

Deutsche Gesellschaft für Luft- und Raumfahrt
Openalex Percentile: Top 62%
Computational Fluid Dynamics and Aerodynamics
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