STELLA: Results of Two Years’ Operation for Megabit/Sec Data Transmission
Overview of the Hybrid RANS Code TAU
Block Structured Navier-Stokes Solver FLOWer
Shape Parametrization Using Freeform Deformation
Computation of Engine-Airframe Installation Drag
Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW
Algorithmic Developments in TAU
Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers
Transition Modeling in FLOWer — Transition Prescription and Prediction
The Continuous Adjoint Approach in Aerodynamic Shape Optimization
Transition Prediction for 2D and 3D Flows using the TAU-Code and N-Factor Methods
Hybrid unstructured Grid Generation in MEGAFLOW
Large-Eddy Simulation of Attached Airfoil Flow
Application of the Adjoint Technique with the Optimization Framework Synaps Pointer Pro
MEGAFLOW for AIRBUS-D — Applications and Requirements
Verification of MEGAFLOW-Software for High Lift Applications
Turbulence Model Implementation in TAU
Advanced Turbulence Modelling in Aerodynamic Flow Solvers