TAU

Overview of the hybrid RANS code TAU. A brief introduction is given which first describes the history of frame in which the TAU code was developed before explaining the main advantages which were the drivers for the selection of the approach. In the following an algorithmic overview describes shortly the code functionality before a section about the code design gives some more insight about the implementation and its scripting capability.


References in zbMATH (referenced in 41 articles , 1 standard article )

Showing results 1 to 20 of 41.
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  1. Wasserman, M.; Mor-Yossef, Y.; Greenberg, J.B.: A positivity-preserving, implicit defect-correction multigrid method for turbulent combustion (2016)
  2. Stück, Arthur: An adjoint view on flux consistency and strong wall boundary conditions to the Navier-Stokes equations (2015)
  3. Langer, Stefan: Agglomeration multigrid methods with implicit Runge-Kutta smoothers applied to aerodynamic simulations on unstructured grids (2014)
  4. Brandfass, B.; Alrutz, T.; Gerhold, T.: Rank reordering for MPI communication optimization (2013) ioport
  5. Kowollik, D.; Tini, V.; Reese, S.; Haupt, M.: 3D fluid-structure interaction analysis of a typical liquid rocket engine cycle based on a novel viscoplastic damage model (2013)
  6. Rosenbaum, Benjamin; Schulz, Volker: Efficient response surface methods based on generic surrogate models (2013)
  7. Zimmermann, R.: On the maximum likelihood training of gradient-enhanced spatial Gaussian processes (2013)
  8. Auerswald, Torsten; Bange, Jens; Knopp, Tobias; Weinman, Keith; Radespiel, Rolf: Large-Eddy Simulations of realistic atmospheric turbulence with the DLR-TAU-code initialized by in situ airborne measurements (2012)
  9. Borzì, Alfio; Schulz, Volker: Computational optimization of systems governed by partial differential equations (2012)
  10. Langer, Stefan: Investigation and application of point implicit Runge-Kutta methods to inviscid flow problems (2012)
  11. Michler, Andreas K.; Heinrich, Ralf: Surrogate-enhanced simulation of aircraft in trimmed state (2012)
  12. Rosenbaum, Benjamin; Schulz, Volker: Comparing sampling strategies for aerodynamic kriging surrogate models (2012)
  13. Michler, Andreas K.: Aircraft control surface deflection using RBF-based mesh deformation (2011)
  14. Özkaya, Emre; Gauger, Nicolas R.: Automatic transition from simulation to one-shot shape optimization with Navier-Stokes equations (2010)
  15. Zimmermann, Ralf; Han, Zhong-Hua: Simplified cross-correlation estimation for multi-fidelity surrogate cokriging models (2010)
  16. Berggren, Martin; Ekstrom, Sven-Erik; Nordstrom, Jan: A discontinuous Galerkin extension of the vertex-centered edge-based finite volume method (2009)
  17. Eriksson, Sofia; Nordström, Jan: Analysis of the order of accuracy for node-centered finite volume schemes (2009)
  18. Krimmelbein, N.; Radespiel, R.: Transition prediction for three-dimensional flows using parallel computation (2009)
  19. Roszak, R.; Posadzy, P.; Stankiewicz, W.; Morzyński, M.: Fluid-structure interaction for large scale complex geometry and nonlinear properties of structure (2009)
  20. Swanson, R.C.; Rumsey, C.L.: Computation of circulation control airfoil flows (2009)

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Further publications can be found at: http://tau.dlr.de/literature/