The European project ATAAC is dedicated to advanced turbulence modeling. The DLR F15 3-element-airfoil test case is one of the so-called application challenges in the framework of this project. For this test case the focus was on hybrid RANS/LES models. Several partners contributed their results using different hybrid approaches. The presentations shows the comparison of all final results
The objective of the joint research project HINVA (High-Lift In-Flight Validation) funded by the Ger...
The paper aims to assess the feasibility of locally turbulence-resolving flow simulations for a high...
The aerodynamic analysis on the DLR-F11 high lift configuration model has been performed on the supe...
This paper presents the European collaborative project “Advanced Turbulence simulation for Aerodynam...
This paper presents the European collaborative project “Advanced Turbulence simulation for Aerodynam...
This paper presents results and lessons learned from the European collaborative project “Advanced Tu...
This paper presents results and lessons learned from the European collaborative project “Advanced Tu...
The current DLR Computational Fluid Dynamics validation activities in the framework of the AIAA Drag...
Hybrid RANS/LES simulations of the DLR-F15 three-element airfoil flow near stall conditions were con...
This paper deals with the validation of turbulence models in the frame work of the DLR-TAU Code, a N...
An overview of the hybrid RANS/LES methodologies developed and applied at DLR (German Aerospace Cent...
Summarization: In this study the development and assessment of an academic CFD (Computational Fluid ...
The contribution of DLR to the numerical flow simulation activities "assessment and improvement...
This work describes the development, implementation and preliminary stages of validation of well-kno...
A study on turbulence theory and modeling is conducted in the first and second part of this work. Th...
The objective of the joint research project HINVA (High-Lift In-Flight Validation) funded by the Ger...
The paper aims to assess the feasibility of locally turbulence-resolving flow simulations for a high...
The aerodynamic analysis on the DLR-F11 high lift configuration model has been performed on the supe...
This paper presents the European collaborative project “Advanced Turbulence simulation for Aerodynam...
This paper presents the European collaborative project “Advanced Turbulence simulation for Aerodynam...
This paper presents results and lessons learned from the European collaborative project “Advanced Tu...
This paper presents results and lessons learned from the European collaborative project “Advanced Tu...
The current DLR Computational Fluid Dynamics validation activities in the framework of the AIAA Drag...
Hybrid RANS/LES simulations of the DLR-F15 three-element airfoil flow near stall conditions were con...
This paper deals with the validation of turbulence models in the frame work of the DLR-TAU Code, a N...
An overview of the hybrid RANS/LES methodologies developed and applied at DLR (German Aerospace Cent...
Summarization: In this study the development and assessment of an academic CFD (Computational Fluid ...
The contribution of DLR to the numerical flow simulation activities "assessment and improvement...
This work describes the development, implementation and preliminary stages of validation of well-kno...
A study on turbulence theory and modeling is conducted in the first and second part of this work. Th...
The objective of the joint research project HINVA (High-Lift In-Flight Validation) funded by the Ger...
The paper aims to assess the feasibility of locally turbulence-resolving flow simulations for a high...
The aerodynamic analysis on the DLR-F11 high lift configuration model has been performed on the supe...