Literature

[12] T. Alrutz," Investigation of the parallel performance of the unstructured DLR-TAU-Code on distributed computing systems", to appear in Proceedings of Parallel CFD 2005, Elsevier, 2006

[18] T. Alrutz, Hybrid Grid Adaptation in TAU, , in: N. Kroll, J.K. Faßbender, (Eds.), "MEGAFLOW - Numerical Flow Simulation for Aircraft Design", Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), 89, Springer pp.163 - 178, ISBN

[11] P. Aumann, H. Barnewitz, K. Becker, R. Heinrich, B. Roll, M. Galle, N. Kroll, T. Gerhold, D. Schwamborn, M. Franke, "MEGAFLOW: Parallel Complete Aircraft CFD", Parallel Computing, Vol. 27, 415-440, 2001

[13] A. Beckert, T. Gerhold, G. Günther, D. Schwamborn, K. Weinman, "Application of the DLR-TAU Code to Fluid-Structure Interaction on Hybrid Grids", Proceedings of ECCOMAS 2000, Barcelona, 11.-14. September 2000

Brodersen, M. Rakowitz, S. Amant, P. Larrieu, D. Destarac, M. Sutcliffe: "Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop", AIAA Journal of Aircraft, Vol. 42, No. 4, pp. 932-940, 2005

[7] CentaurSoft, "CENTAUR", www.centaursoft.com

[17] R. Dwight, "A Comparison of Implicit Algorithms for the Navier-Stokes Equations on Unstructured Grids", Proceedings of the ICCFD Conference, Toronto, Canada, 2004

[14] G.Einarsson, A. Schütte, A. Raichle, B. Schöning, W. Mönnich, J. Neumann, J. Arnold, T. Alrutz, J. Heinecke, T. Forkert, H. Schumann, "Prediction of the Unsteady Behavior of Maneuvering Aircraft by CFD Aerodynamic, Flight-Mechanic and Aeroelastic Coupling", RTO (eds.), AVT-Symposium, Budapest, 2005-04-26, 2005O.

B. Eisfeld, O. Brodersen, "Advanced Turbulence Modelling and Stress Analysis for the DLR-F6 Configuration", AIAA Paper 2005-4727, 2005

[9] M. Galle. T. Gerhold, J. Evans, "Parallel Computation of Turbulent Flows around Complex Geometries on Hybrid Grids with the DLR-TAU Code", A. Ecer, D.R. Emerson (eds.), Proc. 11th Parallel CFD Conf., 23-26 May 1999, Williamsburg, VA, North Holland, 1999.

[2] T. Gerhold, O. Friedrich, J Evans, M. Galle, "Calculation of Complex Three-Dimensional Configurations Employing the DLR-TAU-Code", AIAA-paper 97-0167, 1997

[3] T. Gerhold, V. Hannemann, D. Schwamborn, On the Validation of the DLR-TAU Code, in W. Nitsche H.-J. Heinemann, R. Hilbig (Eds.), "New Results in Numerical and Experimental Fluid Mechanics, Notes on Numerical Fluid Mechanics", 72, Vieweg, S. 426 - 433, ISBN 3-528-03122-0, 1999

[21] T. Knopp, T. Alrutz, D. Schwamborn, "A grid and flow adaptive wall-function method fro RANS turbulence modelling", accepted for Journal of Computational Physics, 2006

[23] J. C. Kok, H.S. Dol, B. Oskam, H.van der Ven, "Extra-Large Eddy Simulation of Massively Separated Flows", AIAA-Paper, 2004-0264 (2004)

[4] N. Kroll and J.K. Fassbender (Eds.), "MEGAFLOW – Numerical Flow Simulation for Aircraft Design, Notes on Numerical Fluid Mechanics and Multidisciplinary Design", Volume 89, Springer (2005)

[5] N. Kroll, C.-C. Rossow, D., Schwamborn, K. Becker, G. Heller, "MEGAFLOW - A Numerical Flow Simulation Tool For Transport Aircraft Design", ICAS Congress 2002, Toronto (can), 09.-13.09.2002, ICAS, CD-Rom, S. 1.105.1-1.105.20, (2002)

[6] N. Kroll, C.-C. Rossow, D. Schwamborn, "The MEGAFLOW-Project - Numerical Flow Simulation for Aircraft. In A. DiBucchianico", R.M.M. Mattheij, M.A. Peletier (Eds.), Progress in Industrial Mathematics at ECMI 2004, Springer, New York, S. 3 – 33, 2005

[10] N. Kroll, Th. Gerhold, S. Melber, R. Heinrich, Th. Schwarz, B. Schöning, "Parallel Large Scale Computations for Aerodynamic Aircraft Design with the German CFD System MEGAFLOW", Parallel CFD 2001, Egmond aan Zee, The Netherlands, May 21-23, 2001

[24] A.Mack, V.Hannemann, "Validation of the Unstructured DLR TAU-Code for Hypersonic Flows", AIAA 2002-3111, 2002

[19] A. Madrane, R. Heinrich, T. Gerhold, "Implementation of the chimera method in the unstructured hybrid DLR finite volume TAU-Code", 6th Overset Composite Grid and Solution Technology Symposium, Ft. Walton Beach, Florida, USA, October 8-10, 2002, www.arl.hpc.mil/Overset2002/contents.html

[8] D. G. Martineau, S. Stokes, S. J. Munday, A. P. Jackson, B. J. Gribben, "Anisotropic Hybrid Mesh Generation for Industrial RANS Applications", AIAA-paper 2006-534, AIAA Aerospace Conference, Reno, 2006

P. Reynier, J. M. Longo, E. Schülein, "Simulation of Missiles with Grid Fins Using an Actuator Disk", JOURNAL OF SPACECRAFT AND ROCKETS, Vol. 43, No. 1, January–February 2006

M. Robinson, K. Hannemann, "Short Duration Force Measurements in Impulse Facilities", AIAA ....

[20] T. Rung, H. Lübcke, M. Franke, L. Xue, F. Thiele, S. Fu, "Assessment of Explicit Algebraic Stress Models in Transonic Flows", Proceedings of the 4th Symposium on Engineering Turbulence Modeling and Measurements, France, pp. 659-668 (1999)

[15] A. Schütte, G. Einarsson, A. Madrane, B. Schöning, W. Mönnich, W.-R. Krüger, "Numerical Simulation of Maneuvering Aircraft by CFD Aerodynamic and Flight-Mechanic Coupling", RTO-AVT Symposium 2002, Paris 22.-24.04.2002

[1] D. Schwamborn, T. Gerhold, R. Heinrich, "The DLR TAU-Code: Recent Applications in Research and Industry", Invited Lecture in Proceedings on CD of the European Conference on Computational Fluid Dynamics ECCOMAS CDF 2006, P. Wesseling, E. Oñate, J. Périaux (Eds), The Netherland, 2006

[22] M. Shur, P. Spalart, M. Strelets, A. Travin, "Detached Eddy simulation of an airfoil at high angle of attack", In: Rodi, W. and Laurence, D. (ed.), Proc. 4Th Int. Sym. Eng. Turb. Modelling and Measurements, Elsevier, Amsterdam, pp 669-678, 1999.

J. Steelant, A. Mack, K. Hannemann, A.D. Gardner, "Comparison of Supersonic Combustion Tests with Shock Tunnels, Flight and CFD", AIAA paper 2006-4684

[16] V. Hannemann, "Structured multigrid agglomeration on a data structure for unstructured meshes", International Journal for Numerical Methods in Fluids, 40, 361-368, 2002

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