The evolution of maximum lift coefficient of a transport aircraft as a function of Reynolds number can be linked to modifications of the laminar-turbulent transition process. In the framework of European project EUROLIFT (I), a task was dedicated to the physical understanding and the numerical modeling of the transition process in high-lift configurations. Then, in the follow-on project EUROLIFT II, a major step is the integration of transition prediction tools within Reynolds-averaged Navier-Stokes (RANS) solvers in order to estimate the impact of transition on performance. This paper presents an overview of the different activities dealing with transition in the EUROLIFT II project
The paper describes an evaluation of the experimental evidence for the DLR-F11 high lift configurati...
In order to enhance its capabilities to handle flows with transition a RANS solver has been extended...
The work reported in this technical report has been carried out in the work package ‘WP3 – Methods &...
The evolution of maximum lift coefficient of a transport aircraft as a function of Reynolds number c...
This paper presents experimental and numerical studies on the effect of the Reynolds number on trans...
A Reynolds-averaged Navier-Stokes (RANS) solver, a laminar boundary layer code and an eN-database me...
The major purpose of the European High Lift Programme EUROLIFT is a common assessment of CFD code ca...
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition pre...
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition pre...
This report has been made during the European project HiAer - High Level Modeling of High Lift Aerod...
Abstract. This contribution highlights development, validation, and application of European CFD code...
A Reynolds-averaged Navier-Stokes solver has been equipped with two different transition prediction ...
The paper will present the key results and the main achievements, as obtained through the challengin...
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition pre...
The modeling of laminar-turbulent transition in RANS flow solvers is an inevitable requirement for t...
The paper describes an evaluation of the experimental evidence for the DLR-F11 high lift configurati...
In order to enhance its capabilities to handle flows with transition a RANS solver has been extended...
The work reported in this technical report has been carried out in the work package ‘WP3 – Methods &...
The evolution of maximum lift coefficient of a transport aircraft as a function of Reynolds number c...
This paper presents experimental and numerical studies on the effect of the Reynolds number on trans...
A Reynolds-averaged Navier-Stokes (RANS) solver, a laminar boundary layer code and an eN-database me...
The major purpose of the European High Lift Programme EUROLIFT is a common assessment of CFD code ca...
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition pre...
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition pre...
This report has been made during the European project HiAer - High Level Modeling of High Lift Aerod...
Abstract. This contribution highlights development, validation, and application of European CFD code...
A Reynolds-averaged Navier-Stokes solver has been equipped with two different transition prediction ...
The paper will present the key results and the main achievements, as obtained through the challengin...
A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition pre...
The modeling of laminar-turbulent transition in RANS flow solvers is an inevitable requirement for t...
The paper describes an evaluation of the experimental evidence for the DLR-F11 high lift configurati...
In order to enhance its capabilities to handle flows with transition a RANS solver has been extended...
The work reported in this technical report has been carried out in the work package ‘WP3 – Methods &...