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
Algorithmic Developments in TAU
Computation of Engine-Airframe Installation Drag
The Continuous Adjoint Approach in Aerodynamic Shape Optimization
Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW
Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers
Transition Modeling in FLOWer — Transition Prescription and Prediction
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
Application of the MEGAFLOW Software at DLR