The DLR TAU-Code: Recent Applications in Research and Industry

By D. Schwamborn, T. Gerhold, R. Heinrich. 2006

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Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function (2013, background): “[32] through [35]) and the discrete TAU adjoint Euler solver (see Refs.”
Modelling of turbulent flow over porous media using a volume averaging approach and a Reynolds stress model (2015, methodology): “All computations accomplished with the adapted version of the DLR TAU-code [28] are obtained by using a second-order central scheme for the mean-flow inviscid fluxes and a first-order upwind Roe scheme for the turbulent fluxes.”
Aircraft control surface deflection using RBF‐based mesh deformation (2011, methodology): “Rather than to relate the influence domain of mesh deformation to a single point, they used wall distances, calculated by their flow solver TAU [39], such that the influence domain was better adapted to the component’s shape.”
Three-Dimensional Large-Scale Aerodynamic Shape Optimization Based on Shape Calculus (2013, background): “More details and validations of TAU can be found in [36,37].”