Overview of the Hybrid RANS Code TAU
Block Structured Navier-Stokes Solver FLOWer
Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW
Shape Parametrization Using Freeform Deformation
The Continuous Adjoint Approach in Aerodynamic Shape Optimization
Advanced Turbulence Modelling in Aerodynamic Flow Solvers
Algorithmic Developments in TAU
Hybrid unstructured Grid Generation in MEGAFLOW
Computation of Engine-Airframe Installation Drag
Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers
Transition Prediction for 2D and 3D Flows using the TAU-Code and N-Factor Methods
MEGAFLOW for AIRBUS-D — Applications and Requirements
Transition Modeling in FLOWer — Transition Prescription and Prediction
G.I.G. — A Flexible User-Interface for CFD-Code Configuration Data
Verification of MEGAFLOW-Software for High Lift Applications
Large-Eddy Simulation of Attached Airfoil Flow
Application of the Adjoint Technique with the Optimization Framework Synaps Pointer Pro
Application of the MEGAFLOW Software at DLR