Intro; Preface; Contents; Review on High-Lift Systems for Aerodynamic Applications; 1 Introduction; 2 Trailing Edge Devices; 3 Leading Edge Devices; 4 Physics of High-Lift Systems and Numerical Simulations; References; Grid Generation About High-Lift Wing Configurations; 1 Introduction; 2 CAD Model; 3 Mesh Generation Guidelines; 4 Surface Mesh Generation; 4.1 Farfield and Symmetry Plane; 4.2 Grid Quality; 4.3 Deviation from HiLiftPW3 Meshing Guidelines; 5 Volume Grid Generation; 6 Final Remarks; References; Incompressible Solutions About High-Lift Wing Configurations; 1 Introduction

2 Numerical Approach3 Grid Generation; 4 Solution Process; 5 Results and Discussion; 5.1 Force and Moment Comparisons; 5.2 Pressure Comparisons; 6 Conclusions and Future Work; References; Numerical Investigations of the Jaxa High-Lift Configuration Standard Model with MFlow Solver; 1 Introduction; 2 Geometry and Computational Grids; 3 Numerical Methods; 4 Results; 4.1 The Performance of Massively Parallel Computing; 4.2 The Effects of Nacelle and Pylon Assembled; 5 Conclusions; References; Time-Resolved Adaptive Direct FEM Simulation of High-Lift Aircraft Configurations; 1 Introduction

2 Simulation Methodology2.1 The cG(1)cG(1) Method; 2.2 The Adaptive Algorithm; 2.3 A Posteriori Error Estimate for cG(1)cG(1); 2.4 The Do-Nothing Error Estimate and Indicator; 2.5 Turbulent Boundary Layers; 2.6 Numerical Tripping; 2.7 The FEniCS-HPC Finite Element Computational Framework; 3 Results; 3.1 Aerodynamic Forces; 3.2 Pressure Coefficients; 3.3 Flow and Adaptive Mesh Refinement Visualization; 4 Conclusions; References; RANS Simulations of the High Lift Common Research Model with Open-Source Code SU2; 1 Introduction; 2 NASA's Common Research Model; 3 Numerical Methods

3.1 Stanford University Unstructured (SU2)3.2 Turbulence Modelling; 3.3 Computational Resources; 3.4 Geometry Description and Grids; 3.5 Geometry; 4 Results and Discussion; 5 Conclusions; References