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
The Continuous Adjoint Approach in Aerodynamic Shape Optimization
Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW
Algorithmic Developments in TAU
Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers