Computations of lift and drag polars for a transport aircraft wing/fuselage high lift configurations using the block-structured and hybrid MEGAFLOW code system (FLOWer/Tau) are carried out and compared to windtunnel experiments
Summarization: In this study the development and assessment of an academic CFD (Computational Fluid ...
This work is dedicated to the investigation of the resolution requirements for hybrid RANS/LES simul...
An overview of the hybrid RANS/LES methodologies developed and applied at DLR (German Aerospace Cent...
Computations of lift and drag polars for a transport aircraft wing/fuselage high lift configuration ...
This paper presents the numerical simulation and the analysis of viscous high-lift flows around a co...
This part of the MEGAFLOW project is concerned with the numerical simulation of the viscous compress...
This report presents first results in the application of the DLR TAU-code to the topic of engine/air...
The application of CFD methods for the solution of the Euler and Reynolds-averaged Navier-Stokes equ...
Numerical results of the solution of the Reynolds-averaged Navier-Stokes equations (RANS)for a compl...
This paper presents the numerical simulation and the analysis of viscous high-lift flows around a co...
The paper aims to assess the feasibility of locally turbulence-resolving flow simulations for a high...
The accuracy of the DLR structured and unstructured computational fluid dynamics (CFD) codes predict...
We present hybrid RANS/LES simulations of the JAXA Standard Model high-lift configuration at near-st...
Hybrid RANS/LES simulations of the Common Research Model in high-lift configuration are presented, w...
Insights and lessons learned from the aerodynamic analysis of a High Wing Transport high-lift config...
Summarization: In this study the development and assessment of an academic CFD (Computational Fluid ...
This work is dedicated to the investigation of the resolution requirements for hybrid RANS/LES simul...
An overview of the hybrid RANS/LES methodologies developed and applied at DLR (German Aerospace Cent...
Computations of lift and drag polars for a transport aircraft wing/fuselage high lift configuration ...
This paper presents the numerical simulation and the analysis of viscous high-lift flows around a co...
This part of the MEGAFLOW project is concerned with the numerical simulation of the viscous compress...
This report presents first results in the application of the DLR TAU-code to the topic of engine/air...
The application of CFD methods for the solution of the Euler and Reynolds-averaged Navier-Stokes equ...
Numerical results of the solution of the Reynolds-averaged Navier-Stokes equations (RANS)for a compl...
This paper presents the numerical simulation and the analysis of viscous high-lift flows around a co...
The paper aims to assess the feasibility of locally turbulence-resolving flow simulations for a high...
The accuracy of the DLR structured and unstructured computational fluid dynamics (CFD) codes predict...
We present hybrid RANS/LES simulations of the JAXA Standard Model high-lift configuration at near-st...
Hybrid RANS/LES simulations of the Common Research Model in high-lift configuration are presented, w...
Insights and lessons learned from the aerodynamic analysis of a High Wing Transport high-lift config...
Summarization: In this study the development and assessment of an academic CFD (Computational Fluid ...
This work is dedicated to the investigation of the resolution requirements for hybrid RANS/LES simul...
An overview of the hybrid RANS/LES methodologies developed and applied at DLR (German Aerospace Cent...
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