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
Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers
Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW
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
Turbulence Model Implementation in TAU
Advanced Turbulence Modelling in Aerodynamic Flow Solvers
G.I.G. — A Flexible User-Interface for CFD-Code Configuration Data
Application of the MEGAFLOW Software at DLR