Items where Subject is "Institute of Aerodynamics and Flow Technology > CASE"

A

Abu-Zurayk, Mohammad and Brezillon, Joel (2011) Shape Optimization Using the Aero-structural Coupled Adjoint Approach for Viscous Flows. Eurogen 2011, 13-16 Sep 2011, Capua, Italy.

Abu-Zurayk, Mohammad and Brezillon, Joel (2011) Efficient Aero-Elastic Shape Optimization Using the Discrete Viscous Adjoint. STAB 2011, Göttingen, Germany. Volltext nicht online.

Albensoeder, Stefan and Ballmann, Josef and Barnewitz, Holger and Behr, Marek and Bogdanski, Steffen and Filimon, Alexander and Fritz, Willy and Gauger, Nicolas and Haupt, Matthias and Henes, Daniel and Horst, Peter and Litvinenko, Alexander and Lutz, Thorsten and Matthies, Hermann G. and Mazlum, Ekrem and Meinke, Matthias and Mockett, Charles and Munz, Claus-Dieter and Orlt, Matthias and Radespiel, Rolf and Reich, Paul and Reimer, Lars and Rieger, Herbert and Roidl, Benedikt and Schillings, Claudia and Schmidt, Tobias and Schröder, Wolfgang and Schulz, Volker and Thiele, Frank and Wellmer, Georg and Wolf, Alexander (2010) Verbundprojekt MUNA: Best-Practice-Regeln. DLR-Interner Bericht. 124-2010/5. DLR. 78 S. Volltext nicht online.

Alrutz, Thomas (2005) Hybrid Grid Adaptation in TAU. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 109-116. Springer. Closing Presentation DLR Project MEGAFLOW, 10.-11.12.2002, Braunschweig (Germany). ISBN 3-540-24383-6. Volltext nicht online.

Alrutz, Thomas and Knopp, Tobias (2006) Near-wall grid adaptation for turbulent flows. International Journal of Computing Science and Mathematics. INDERSCIENCE. Volltext nicht online.

Alrutz, Thomas and Knopp, Tobias (2008) Near-wall grid adaption for turbulent flows. International Journal of Computing Science Mathematics (1), pp. 177-192. Volltext nicht online.

Alrutz, Thomas and Ruetten, Markus (2005) Investigation of Vortex Breakdown over a Pitching Delta Wing applying the DLR TAU-Code with Full, Automatic Grid Adaptation. AIAA. 35th AIAA Fluid Dynamics, 6-9 June 2005, Toronto, Canada. Volltext nicht online.

Alrutz, Thomas and Vollmer, Daniel (2010) Recent Developments of TAU Adaptation Capability. In: MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 107. Springer Verlag Berlin, Heidelberg. pp. 3-19. ISBN 978-3-642-04092-4. ISSN 1612-2909. Volltext nicht online.

Alrutz, Thomas (2005) Investigation of the parallel performance of the unstructured DLR-TAU-Code on distributed computing systems. In: Proceedings of Parallel CFD 2005, pp. 509-516. Elsevier, The Netherlands. International Conference of Parallel Computational Fluid Dynamics 2005, 24-05-2005 - 27-05-2005, Washington, DC (USA). ISBN 978-0-444-52206-1. ISSN 1570-9426. Volltext nicht frei.

Alrutz, Thomas and Knopp, Tobias (2006) Near wall grid adaption for wall functions. In: Proceedings of International Conference on Boundary and Interior Layers 2006. University of Goettingen. BAIL 2006, 2006-07-24 - 2006-07-28, Goettingen, Germany. Volltext nicht frei.

Alrutz, Thomas and Orlt, Matthias (2006) Parallel dynamic grid refinement for industrial applications. In: Proceedings ECCOMAS CFD 06. TU Delft, The Netherlands. ECCOMAS CFD 06, 2006-09-05 - -2006-09-08, Egmond aan Zee, The Netherlands. ISBN 90-9020970-0. Volltext nicht frei.

Andres-Perez, Esther and Widhalm, Markus and Caloto, Aitor (2009) Achieving High Speed CFD simulations: Optimization, Parallelization, and FPGA Acceleration for the unstructured DLR TAU Code. AIAA 47th Aerospace Science Meeting, [2009-01-05 - 2009-01-08] AIAA-2009-0759, Orlando, FL (USA).

Arthur, Malcolm and Dol, Henry and Krumbein, Andreas and Houdeville, Robert and Ponsin, Jorge (2003) Application of Transition Criteria in Navier-Stokes Computations. Project Report. TP137. (Unpublished) Volltext nicht frei.

B

Bangerth, Wolfgang and Hartmann, Ralf and Guido, Kanschat (2007) deal.II --- a General Purpose Object Oriented Finite Element Library. ACM Transactions on Mathematical Software, 33 (4), p. 24.

Bassi, Francesco and De Bartolo, Carmine and Hartmann, Ralf and Nigro, Alessandra (2009) A discontinuous Galerkin method for inviscid low Mach number flows. Journal of Computational Physics, 228 (11), pp. 3996-4011. Elsevier. doi: 10.1016/j.jcp.2009.02.021. ISSN 0021-9991.

Beaumier, Philippe and Chelli, Enrico and Pahlke, Klausdieter (2001) Navier-Stokes Prediction of Helicopter Rotor Performance Including Aero-Elastic Effects. Journal of the American Helicopter Society, 46 (4). AMERICAN HELICOPTER SOCIETY INCORPORATION. ISSN 0002-8711. Volltext nicht online.

Brandfass, Barbara (2010) Optimierung der MPI-Prozess-Kommunikation bei Multicore-Rechnerarchitekturen mit Hilfe des quadratischen Zuordnungsproblems. DLR-Interner Bericht. DLR-IB 224-2011 A 60. Diploma.

Brezillon, Joel and Dwight, Richard (2005) Discrete Adjoint of the Navier-Stokes Equations for Aerodynamic Shape Optimization. EUROGEN 2005 - Sixth Conference on Evolutionary and Deterministic Methods for Design, Optimization and Control with Applications to Industrial and Societal Problems, 2005-09-12 2005-09-14, Munich, Germany.

Brezillon, Joel and Wild, Jochen (2005) Evaluation of Different Optimization Strategies for the Design of a High-Lift Flap Device. EUROGEN 2005 - Sixth Conference on Evolutionary and Deterministic Methods for Design, Optimization and Control with Applications to Industrial and Societal Problems, 2005-09-12 2005-09-14, Munich, Germany.

Brodersen, Olaf and Eisfeld, Bernhard and Raddatz, Jochen and Frohnapfel, Petra (2008) DLR Results from the Third AIAA Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 45 (3), pp. 823-836. doi: 10.2514/1.30628. ISSN 0021-8669. Volltext nicht online.

Bugeda, Gabriel and Courty, J.-C. and Gilliot, Anne and Höld, Roland and Marini, Marco and Nguyen, T. van and Papailiou, Kyriakos and Periaux, Jacques and Schwamborn, Dieter (2006) Verification and Validation Methods for Challenging Multiphysics Problems. A Series of Handbooks on Therory and Engineering Applications of Computational Methods. CIMNE Barcelona, Spain. ISBN 84-96736-00-8. Volltext nicht online.

Bugeda, Gabriel and Courty, Jean-Claude and Gilliot, Anne and Höld, Roland and Marini, Marco and Nguyen, Toan and Papailiou, Kyriakos and Periaux, Jacques and Schwamborn, Dieter (2006) Verfication and Validation Methods for Challenging Multiphysics Problems. A Series of Handbook on Theory and Engineering Applications of Computational Methods. International Center for Numerical Methods in Engineering (CIMNE). ISBN 84-96736-00-8. Volltext nicht online.

Bunge, U. and Mockett, B. and Aupiox, B. and Haase, W. and Menter, F. and Schwamborn, Dieter and Weinman, Keith (2006) Summary of experience. In: NNFM Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 94. Springer Verlag. pp. 405-420. ISBN 3-540-28786-8. Volltext nicht online.

C

Crippa, Simone (2010) Numerical Aspects of NASA Trap-Wing Computations using the DLR TAU Code. First AIAA High Lift Prediction Workshop, 26-27 Jun 2010, Chicago, IL, USA. (Unpublished)

Crippa, Simone (2010) Application of Novel Hybrid Mesh Generation Methodologies for Improved Unstructured CFD Simulations. In: Conference Procedings. 28th AIAA Applied Aerodynamics Conference, 28 Jun - 01 Jul 2010, Chicago, IL, USA.

Crippa, Simone (2011) Improvement of Unstructured Computational Fluid Dynamics Simulations Through Novel Mesh Generation Methodologies. Journal of Aircraft, 48 (3), pp. 1036-1044. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C031219. ISSN 0021-8669.

Crippa, Simone and Krimmelbein, Normann (2011) Transitional Flow Computations of the NASA Trapezoidal Wing. In: Jahresbericht 2011, pp. 104-105. 15. STAB Workshop, 9-10 Nov 2011, Göttingen.

D

Dietz, Markus and Khier, Walid and Knutzen, Bjoern and Wagner, Siegfried and Krämer, Ewald (2008) Numerical Simulation of a Full Helicopter Configuration Using Weak Fluid-Structure Coupling. 46th AIAA Aerospace Sciences Meeting and Exhibit., 2008-01-07, Reno (USA).

Dwight, Richard (2007) Goal-Oriented Mesh Adaptation using a Dissipation-Based Error Indicator. International Journal of Numerical Methods in Fluids. doi: 10.1002/fld.1582.

Dwight, Richard (2007) Adjoint Algorithms for the Optimization of 3d Turbulent Configurations. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 96. Springer.

Dwight, Richard (2006) Robust Mesh Deformation using the Linear Elasticity Equations. Computational Fluid Dynamics. Springer.

Dwight, Richard (2004) Time-Accurate Navier-Stokes Calculations with Approximately Factored Implicit Schemes. Computational Fluid Dynamics. Springer. ISBN 3540318003.

Dwight, Richard (2007) A Posteriori Estimation of Error due to Dissipation in Finite Volume Schemes and Application to Mesh Adaptation. In: AIAA Paper Series (AIAA-2007-4093). AIAA. AIAA CFD Conference, 2007-06, Miami, USA.

Dwight, Richard (2006) Efficiency Improvements of RANS-Based Analysis and Optimization using Implicit and Adjoint Methods on Unstructured Grids. DLR-Forschungsbericht. DLR FB-2006-11. Dissertation. University of Manchester.

Dwight, Richard (2006) Engine Inflow Boundary Conditions for Specification of Mass Flow. DLR-Interner Bericht. DLR IB 124-2006/6.

Dwight, Richard and Brezillon, Joel (2006) Effect of Approximations of the Discrete Adjoint on Gradient-Based Optimization. AIAA Journal, 44 (12), pp. 3022-3071.

Dwight, Richard and Brezillon, Joel (2007) Adjoint Algorithms for the Optimization of 3d Turbulent Configurations. In: 2006 STAB, 96. Springer. STAB 2006, 2006-10, Darmstadt.

Dwight, Richard and Brezillon, Joel (2008) Efficient and Robust Algorithms for Solution of the Adjoint Compressible Navier–Stokes Equations with Applications. International Journal for Numerical Methods in Fluids (60), pp. 365-389. Wiley InterScience. doi: 10.1002/fld.1894.

Dwight, Richard and Brezillon, Joel and Vollmer, Daniel (2006) Efficient Algorithms for Solution of the Adjoint Compressible Navier-Stokes Equations with Applications. In: ODAS 2006. ODAS 2006, 2006, Toulouse, France.

E

Eisfeld, Bernhard (2002) Die Reynolds-Spannungsgleichungen für kompressible Strömung - Herleitung und Zusammenhänge. DLR-Interner Bericht. DLR-IB 124-2002/36. 52 S. Volltext nicht online.

Eisfeld, Bernhard (1999) Pseudokontinuierliche Modellierung der Strömung in Schüttschichtreaktoren. Dissertation, Brandenburgische Technische Universität Cottbus. Volltext nicht online.

Eisfeld, Bernhard (2005) Collection of equations for compressible turbulent flow. DLR-Interner Bericht. DLR-IB 124-2005/7. 36 S. Volltext nicht online.

Eisfeld, Bernhard (2004) Numerical simulation of aerodynamic problems with a Reynolds stress turbulence model. Springer. 14. STAB/DGLR-Symposium, 2004-11-16 - 2004-11-18, Bremen. ISBN 3-540-33286-3. Volltext nicht online.

Eisfeld, Bernhard (2006) ONERA M6 wing. In: FLOMANIA - A European Initiative on Flow Physics Modelling Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 94. Springer-Verlag. pp. 219-224. ISBN 3-540-28786-8. Volltext nicht online.

Eisfeld, Bernhard (2006) Die Thin-Shear-Layer-Approximation zur Berechnung der viskosen Flüsse. DLR-Interner Bericht. DLR-IB 124-2006/7. 53 S. Volltext nicht online.

Eisfeld, Bernhard (2007) Simulation aerodynamischer Probleme mit einem Reynolds-Spannungsmodell. Gemeinsamer Technologietag ERCOFTAC Nord-/Süddeutschland, 2007-10-05, Stuttgart. (Unpublished) Volltext nicht online.

Eisfeld, Bernhard (2008) Der Einfluss der Längenmaßgleichung auf die Simulation aerodynamischer Strömungen mit Reynolds-Spannungsmodellen. 16. DGLR/STAB-Symposium, 2008-11-03 - 2008-11-04, Aachen. (Unpublished) Volltext nicht online.

Eisfeld, Bernhard (2009) Das Verbundprojekt MUNA - Management und Minimierung von Unsicherheiten in der Numerischen Aerodynamik. 14. STAB Workshop, 11-12 Nov 2009, Göttingen. (Unpublished) Volltext nicht online.

Eisfeld, Bernhard (2010) Reynolds Stress Modeling for Complex Aerodynamic Flows. In: Proceedings. 5th European Conference on Computational Fluid Dynamics, ECCOMAS CFD, 14-17 Jun 2010, Lisbon. ISBN 978-989-96778-1-4. Volltext nicht online.

Eisfeld, Bernhard (2010) The German National Joint Project MUNA: Management and Minimization of Uncertainties and Errors in Numerical Aerodynamics. In: Proceedings. 5th European Conference on Computational Fluid Dynamics, ECCOMAS CFD, 14-17 Jun 2010, Lisbon. ISBN 978-989-96778-1-4. Volltext nicht online.

Eisfeld, Bernhard (2011) Numerical Uncertainties and Error Control: The MUNA Project. ERCOFTAC Short Course “Uncertainty Management and Quantification in Industrial Analysis and Design”, 03-04 Mar 2011, Garching. (Unpublished) Volltext nicht online.

Eisfeld, Bernhard (2011) Numerical Uncertainties and Error Control: The MUNA Project. ERCOFTAC Short Course “Uncertainty Management and Quantification in Industrial Analysis and Design”, 15-16 Sep 2011, Hampton, Virginia, USA. (Unpublished) Volltext nicht online.

Eisfeld, Bernhard and Knopp, Tobias and Calvo, Javier Bartolome (2008) Anwendung einer neuen Erweiterung für k-ω-Turbulenzmodelle zur Berücksichtigung von Wandrauhigkeit auf Strömungen mit Ablösung. 16. DGLR/STAB-Symposium, 2008-11-03 - 2008-11-04, Aachen. (Unpublished) Volltext nicht online.

Eisfeld, Bernhard and Rudnik, Ralf (2002) Der Einfluß der Schließungskoeffizienten und der ω-Randbedingung auf die Lösung der RANS-Gleichungen mit dem k-ω-Turbulenzmodell von Wilcox bei transsonischer Strömung. DLR-Interner Bericht. DLR-IB 124-2002/35. 27 S. Volltext nicht online.

Eisfeld, Bernhard and Spiering, Frank (2011) Untersuchung des Einflusses der Deformation und des Turbulenzmodells auf Simulationsergebnisse am Beispiel der HiReTT-Konfiguration. 15. DGLR/STAB-Workshop, 09-10 Nov 2011, Göttingen. (Unpublished)

Eisfeld, Bernhard and Weinman, Keith and Schwamborn, Dieter (2006) DLR´s Contribution to FLOMANIA - Methods, Models, Applications. In: NNFM Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 94. Springer Verlag. pp. 49-56. ISBN 3-540-28786-8. Volltext nicht online.

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Fassbender, Jens K. (2005) Robust and efficient computation of turbulent flows around civil transport aircraft at flight Reynolds numbers. Aerospace Science and Technology, 9 (8), pp. 672-680. Elsevier. doi: 10.1016/j.ast.2005.09.003. Volltext nicht online.

Faßbender, Heike and Vendl, Alexander and Görtz, Stefan and Zimmermann, Ralf and Mifsud, Michael (2011) More Simulation - Less Testing. In: European Success Stories in Industrial Mathematics Springer. p. 88. ISBN 978-3-642-23847-5. Volltext nicht online.

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Gerhold, Thomas (2002) Overview of the Hybrid Rans Code TAU. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 89. Springer Verlag. pp. 81-92. ISBN 3-540-24383-6. ISSN 1612-2909. Volltext nicht online.

Gerhold, Thomas (2011) Preparing TAU for Many-Cores. Onera Scientific Days , 07. Oct. 2011, Châtillon, France . Volltext nicht online.

Gerhold, Thomas and Evans, John (1999) Efficient Computation of 3D-Flows for Complex Configurations with the DLR-TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics, 72, pp. 178-185. Vieweg. AG STAB Symposium, 1998-11-10 - 1998-11-12, Berlin. ISBN 3-528-03122-0. Volltext nicht online.

Gerhold, Thomas and Neumann, Jens (2007) The parallel mesh deformation of the DLR TAU-Code. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 96. Springer-Verlag Berlin Heidelberg 2007. pp. 162-169. ISBN 3-540-74458-4. Volltext nicht online.

Gerhold, Thomas and Jägersküpper, Jens and Kroll, Norbert (2011) Exascale - Chance & Challenge for CFD in Aircraft Design. International Supercomputing Conference (ISC), 19. – 23. Jun. 2011, Hamburg, Germany. Volltext nicht online.

Gerhold, Thomas and Neumann, Jens (2006) The parallel mesh deformation of the DLR TAU-Code. 15. DGLR-Fach-Symposium der STAB, 2006-11-29-2006-12-01, Darmstadt (Germany). (Submitted) Volltext nicht frei.

Giering, Ralf and Kaminski, Thomas and Eisfeld, Bernhard and Gauger, Nicolas and Raddatz, Jochen and Reimer, Lars (2009) Automatic Differentiation of FLOWer and MUGRIDO. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107. Springer. pp. 221-235. ISBN 978-3-642-04092-4. ISSN 1612-2909. Volltext nicht online.

Görtz, Stefan (2011) Fusing computational and experimental flow data with Gappy POD. Graduiertenkolleg Lorentzkraft, 3. Mai 2011, Ilmenau, Deutschland. Volltext nicht online.

Görtz, Stefan and Mifsud, Michael (2011) Fusing computational and experimental data with Gappy POD for harmonized aerodynamic data. CFD and Experiment – Integration of Simulation Workshop, 5.-6. April 2011, Göttingen, Deutschland. Volltext nicht online.

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Haase, Werner and Aupiox, Bertrand and Bunge, Ulf and Schwamborn, Dieter (2006) FLOMANIA - A European Initiative on Flow Physics Modelling. NNFM, 94. Springer Verlag. 420 S. ISBN 3-540-28786-8. Volltext nicht online.

Han, Zhong-Hua and Zimmermann, Ralf and Görtz, Stefan (2010) A New Cokriging Method for Variable-Fidelity Surrogate Modeling of Aerodynamic Data. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 4-7 Jan 2010, The United States.

Hartmann, Ralf (2006) Adaptive discontinuous Galerkin methods with shock-capturing for the compressible Navier-Stokes equations. International Journal for Numerical Methods in Fluids, 51 (9-10), pp. 1131-1156. John Wiley & Sons.

Hartmann, Ralf (2006) Discontinuous Galerkin methods for compressible flows: higher order accuracy, error estimation and adaptivity. In: VKI Lecture Series, 2006-0. pp. 1-50.

Hartmann, Ralf (2006) Derivation of an adjoint consistent discontinuous Galerkin discretization of the compressible Euler equations. In: BAIL 2006 Conference. BAIL 2006 Conference, 2006-07-24 - 2006-07-28, Goettingen, Germany.

Hartmann, Ralf (2006) Error estimation and adjoint-based adaptation in aerodynamics. In: Proceedings of the ECCOMAS CFD 2006 conference. ECCOMAS CFD 2006, 2006-09-05 - 2006-09-08, Egmond aan Zee, The Netherlands.

Hartmann, Ralf (2006) Discontinuous Galerkin methods for compressible flows: higher order accuracy, error estimation and adaptivity. NIA Workshop on High-Order Methods and High-Fidelity Simulations, 2006-11-06 - 2006-11-07, Hampton, Virginia.

Hartmann, Ralf (2006) Error estimation and adjoint based refinement for an adjoint consistent DG discretization of the compressible Euler equations. Int. J. Computing Science and Mathematics, 1 (2-4), pp. 207-220.

Hartmann, Ralf (2007) DG discretizations for compressible flows: Adjoint consistency analysis, error estimation and adaptivity. Adaptive Numerical Methods for PDEs, 2007-06-10 - 2007-06-16, Oberwolfach.

Hartmann, Ralf (2007) DG methods for aerodynamic flow simulations. ICFD workshop on the Discontinuous Galerkin method and its applications, Institute for Computational Fluid Dynamics (ICFD), University of Reading, 2007-10-31, Reading (UK).

Hartmann, Ralf (2007) Entwicklung von Discontinuous Galerkin Verfahren höherer Ordnung auf unstrukturierten adaptiv verfeinerten Gittern inklusive Fehlerschätzung. STAB workshop 2007, 2007-11-14 - 2007-11-15, Göttingen.

Hartmann, Ralf (2008) Multitarget error estimation and adaptivity in aerodynamic flow simulations. SIAM Journal on Scientific Computing, 31 (1), pp. 708-731.

Hartmann, Ralf (2008) Numerical Analysis of Higher Order Discontinuous Galerkin Finite Element Methods. In: VKI Lecture Series, 2008-0. pp. 1-107. ISBN 13 978-2-930389-88-5.

Hartmann, Ralf (2008) Error estimation and adjoint-based refinement for multiple force coefficients in aerodynamic flow simulations. 5th European Congress on Computational Methods in Applied Sciences and Engineeering (ECCOMAS 2008), 2008-06-30 - 2008-07-05, Venice, Italy.

Hartmann, Ralf (2008) Adaptive Discontinuous Galerkin methods in aerodynamic flow simulations. Conference on Modeling, Simulation and Optimization of Complex Processes (MOSOCOP 08), 2008-07-21 - 2008-07-25, Heidelberg.

Hartmann, Ralf (2008) Numerical Analysis of Higher Order Discontinuous Galerkin Finite Element methods. VKI Lecture Series 2008-08, 2008-10-13 - 2008-10-17, Rhode Saint Genese, Belgium.

Hartmann, Ralf (2010) Adjoint-based error estimation and goal-oriented mesh refinement for aerodynamic flows. ECCOMAS CFD 2010, 14-17 June 2010, Lisbon, Portugal. (Unpublished) Volltext nicht frei.

Hartmann, Ralf (2010) Aerodynamic flow simulations based on deal.II. Workshop on: Recent and Future Development with and of deal.II, 23-25 Aug 2010, Heidelberg. (Unpublished) Volltext nicht frei.

Hartmann, Ralf (2010) Error estimation and adaptive mesh refinement for aerodynamic flows. Oberseminar Numerische Mathematik, Universität Heidelberg, 14 April 2010, Heidelberg. (Unpublished) Volltext nicht frei.

Hartmann, Ralf (2011) DG Methods for Aerodynamic Flows: Higher order, error estimation and adaptive mesh refinement. 16th International Conference on Finite Elements in Flow Problems, 23-25 March 2011, Munich, Germany.

Hartmann, Ralf and Held, J. and Leicht, T. and Prill, F. (2009) ADIGMA final meeting: Error estimation and local mesh refinement for turbulent flows. Closing Workshop of the European Project on Adaptive Higher-Order Variational Methods for Aerodynamic Applications in Industry, 8-10 Dec 2009, Braunschweig. (Unpublished) Volltext nicht frei.

Hartmann, Ralf and Held, Joachim and Leicht, Tobias (2011) Adjoint-based error estimation and adaptive mesh refinement for the RANS and k-ω turbulence model equations. Journal of Computational Physics, 230 (11), pp. 4268-4284. Elsevier. doi: 10.1016/j.ast.2010.04.002. ISSN 0021-9991.

Hartmann, Ralf and Held, Joachim and Leicht, Tobias and Prill, Florian (2010) Error estimation and adaptive mesh refinement for aerodynamic flows. In: Notes on numerical fluid mechanics and multidisciplinary design, 113. Springer. pp. 339-353. ISBN 978-3-642-03706-1. ISSN 1612-2909.

Hartmann, Ralf and Held, Joachim and Leicht, Tobias and Prill, Florian (2010) Discontinuous Galerkin methods for computational aerodynamics - 3D adaptive flow simulation with the DLR PADGE code. Aerospace Science and Technology, 14, pp. 512-519. Elsevier. doi: 10.1016/j.ast.2010.04.002. ISSN 1270-9638.

Hartmann, Ralf and Houston, Paul (2006) Symmetric Interior Penalty DG Methods for the Compressible Navier--Stokes Equations I: Method Formulation. International Journal of Numerical Analysis & Modeling, 3 (1), pp. 1-20.

Hartmann, Ralf and Houston, Paul (2006) Symmetric Interior Penalty DG Methods for the Compressible Navier--Stokes Equations II: Goal--Oriented A Posteriori Error Estimation. International Journal of Numerical Analysis & Modeling, 3 (2), pp. 141-162.

Hartmann, Ralf and Houston, Paul (2008) An optimal order interior penalty discontinuous Galerkin discretization of the compressible Navier-Stokes equations. Journal of Computational Physics, 227 (22), pp. 9670-9685. Elsevier.

Hartmann, Ralf and Houston, Paul (2010) Error estimation and adaptive mesh refinement for aerodynamic flows. In: ,Von Karman Institute for Fluid Dynamics, Rhode Saint Genese, Belgium. ISBN 13 978-2-930389-98-2.

Hartmann, Ralf and Leicht, Tobias (2010) Discontinuous Galerkin Verfahren in der Aerodynamik: Höhere Ordnung, Fehlerschätzung und Gitteradaption. 17. DGLR-Fach-Symposium der STAB, 9-10 Nov 2010, Berlin. (Unpublished) Volltext nicht frei.

Hartmann, Ralf and Leicht, Tobias (2011) DG Methods for Aerodynamic Flows: Higher order, error estimation and adaptive mesh refinement. HONOM 2011, 11-15 April 2011, Trento, Italy.

Hartmann, Ralf and Lukacova-Medvidova, M. and Prill, F. (2009) Efficient Preconditioning for the Discontinuous Galerkin Finite Element Method by Low-Order Elements. Applied Numerical Mathematics, 59 (8), pp. 1737-1753. Elsevier. doi: 10.1016/j.apnum.2009.01.002. ISSN 0168-9274. Volltext nicht online.

Hazra, Subhendu and Schulz, Volker and Brezillon, Joel (2008) Simultaneous Pseudo-Time Stepping for 3D Aerodynamic Shape Optimization. Numerical Mathematics, 16 (Heft 2), pp. 139-161. Walter de Gruyter . doi: 10.1515/JNUM.2008.007. ISSN 1569-3953. Volltext nicht online.

Heinrich, Ralf and Reimer, Lars and Michler, Andreas (2011) Multidisciplinary simulation of maneuvering aircraft interacting with atmospheric effects using the DLR TAU code. RTO AVT-189 Specialists’ Meeting on Assessment of Stability and Control Prediction Methods for Air and Sea Vehicles, 12.-14. Oktober 2011, Portsdown West, UK. Volltext nicht frei.

Held, Joachim (2007) Ein Gebietszerlegungsverfahren für parabolische Probleme im Zusammenhang mit Finite-Volumen-Diskretisierung. Dissertation, Universität Göttingen. Volltext nicht online.

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Jakirlic, Suad and Eisfeld, Bernhard and Basara, Branislav (2009) Performance Assessment of Some Popular RANS Models by Relevance to High-Lift Aerodynamics. In: AIAA-Paper (2009-0049). American Institute of Aeronautics and Astronautics. AIAA Conference, 5-8 Jan 2009, Orlando. Volltext nicht online.

Jakirlic, Suad and Eisfeld, Bernhard and Jester-Zürker, Roland and Tropea, Cameron and Kroll, Norbert (2009) Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models. In: MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107. Springer. pp. 73-92. ISBN 978-3-642-04092-4. ISSN 1612-2909. Volltext nicht online.

Jakirlic, Suad and Eisfeld, Bernhard and Jester-Zürker, Roland and Kroll, Norbert (2007) Near-wall, Reynolds-stress model calculations of transonic flow configurations relevant to aircraft aerodynamics. International Journal of Heat and Fluid Flow, 28, pp. 602-615. Elsevier. doi: 10.1016/.j.heatfluidflow.2007.04.001. Volltext nicht online.

Jakubek, Daria (2010) Parameterstudien für numerische RANS- und DES-Verfahren für ein Drei-Element Profil in Hochauftriebskonfiguration mit dem DLR TAU-CODE. DLR-Interner Bericht. DLR-IB 224-2010 A 39. Diploma. RWTH Aachen. 102 S. Volltext nicht online.

Jester-Zürker, Roland and Jakirlic, Suad and Eisfeld, Bernhard (2006) Near-Wall, Reynolds-Stress Model Calculations of Transonic Flow Configurations Relevant to Aircraft Aerodynamics. In: Proceedings of the Conference on Modelling Fluid Flow (CMFF'06), pp. 264-271. Conference on Modelling Fluid Flow (CMFF'06), 2006-09-06 - 2006-09-09, Budapest. ISBN 963 420 872 X. Volltext nicht online.

Jägersküpper, Jens (2010) DLR's TAU Code on Massively Parallel Architectures - Hybrid MPI/Shared-Memory Parallelization. NAM-Seminar, Göttingen. (Unpublished) Volltext nicht online.

Jägersküpper, Jens (2011) Highly Parallel CFD for External Aerodynamics with DLR's TAU Code. 23rd International Conference on Parallel Computational Fluid Dynamics (ParCFD), 16-20 May 2011, Barcelona, Spain. (Unpublished) Volltext nicht online.

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Karl, Sebastian and Lambert, Markus (2009) CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19.-22. Okt. 2009, Bremen. Volltext nicht online.

Karl, Sebastian and Markus, Lambert (2009) CFD modeling of hypervelocity re-entry flows including gas radiation. 27th International Symposium on Shock Waves, 19.-24. Juli 2009, St. Petersburg (Russia). Volltext nicht online.

Kersken, Hans-Peter and Schreiber, Andreas and Heinrich, Ralf and Kügeler, Edmund and Mack, Andreas and Neumann, Jens and Schäfer, Roger (2002) TENT - Eine Softwareintegrationsumgebung für multidisziplinäre Simulationen. In: Tagungsband Deutscher Luft- und Raumfahrtkongress 2002. Deutscher Luft- und Raumfahrtkongress 2002, 2002-09-26, Stuttgart. Volltext nicht online.

Kessler, Roland and Pennecot, Julien and Rütten, Markus (2008) Simulations of the Flow in a Human Nose. Stab Tagung 2008, 2008-11-02 - 2008-11-04, Aachen. Volltext nicht online.

Kessler, Roland and Rütten, Markus and Pennecot, Julien (2010) Simulation of the Flow in a Human Nose. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112. Springer-Verlag, Berlin Heidelberg. pp. 521-528. doi: 10.1007/978-3-642-14243-7_64. ISBN 978-3-642-14242-0. ISSN 1612-2909. Volltext nicht online.

Knopp, Tobias (2005) A new adaptive wall-function method for subsonic and transonic turbulent flows. DLR-Interner Bericht. DLR-IB 224-2005 A 14. 55 S. Volltext nicht online.

Knopp, Tobias (2006) Validation of the Turbulence Models in the DLR TAU Code for Transonic Flows - A Best Practice Guide. DLR-Forschungsbericht. DLR-FB 2006-01. 106 S. Volltext nicht online.

Knopp, Tobias (2006) Model-consistent universal wall-functions for RANS turbulence modelling. BAIL 2006 International Conference on Boundary and Interior Layers, 24. - 28. Juli 2006, Göttingen, Deutschland. ISBN 3-00-019600-5. Volltext nicht online.

Knopp, Tobias (2008) Validierung eines semi-empirschen Verfahrens für die instationäre Aerodynamik von Profil- und Ruderschwingungen. DLR-Interner Bericht. DLR-IB 224-2008 A 25. 25 S. Volltext nicht online.

Knopp, Tobias (2010) A modification of DDES based on a detection of attached boundary layers and flow separation. 17. DGLR-Fach-Symposium der STAB, 09.-10. Nov. 2010, Berlin, Deutschland.

Knopp, Tobias (2010) A modification of hybrid RANS-LES methods of DES-type for flows around airplane wings. Workshop on Calibration of Viscosity Models for Turbulent Flows, 08. - 09. Oct. 2010, Goettingen, Germany.

Knopp, Tobias and Alrutz, Thomas and Schwamborn, Dieter (2005) A grid and flow adaptive wall-function method for RANS turbulence modelling. Journal of Computational Physics. Volltext nicht online.

Knopp, Tobias and Alrutz, Thomas and Schwamborn, Dieter (2006) A grid and flow adaptive wall-function method for RANS turbulence modelling. Journal of Computational Physics (220), pp. 19-40. Volltext nicht online.

Knopp, Tobias and Schanz, Daniel and Schröder, Andreas and Dumitra, Michnea and Kähler, Christian (2011) Experimental investigation of a turbulent boundary layer flow at high Reynolds number with and without separation. CFD and Experiment – Integration of Simulation, Workshop of the DGLR-Querschnittsbereich Thermo- and Fluiddynamics, 05. - 06. Apr. 2011, Göttingen, Deutschland. Volltext nicht online.

Knopp, Tobias and Schroeder, Andreas and Dumitra, Michnea and Kaehler, Christian (2011) Experimental investigation of a turbulent boundary layer flow at high Reynolds number without and with separation using PIV. Design of the experiment, wall-laws of turbulence, and improvement of RANS models for maximum-lift prediction. CFD and Experiment – Integration of Simulation Workshop of the DGLR-Querschnittsbereich Thermo- and Fluiddynamics , 05. - 06. April 2011, Göttingen, Germany. Volltext nicht frei.

Knopp, Tobias and Zhang, Xiaoqin and Lube, Gert (2010) Assessment of resolution quality for LES. EUROMECH 504 Large Eddy Simulation for Aerodynamics and Aeroacoustics, 23.-25. Mar. 2009, Muenchen; Germany.

Knopp, Tobias (2011) The actuation boundary condition for flow control in the DLR TAU Code. DLR-Interner Bericht. DLR-IB 224-2010 A 44. 28 S. Volltext nicht frei.

Knopp, Tobias (2011) Titel confidential. DLR-Interner Bericht. DLR-IB 224–2011 C 106. 56 S. Volltext nicht frei.

Knopp, Tobias and Eisfeld, Bernhard and Bartolome Calvo, Javier (2009) A new extension for k-omega turbulence models to account for wall roughness. International Journal of Heat and Fluid Flow, 30 (1), pp. 54-65. Elsevier. doi: 10.1016/j.ijheatfluidflow.2008.09.009. Volltext nicht frei.

Knopp, Tobias and Zhang, Xiaoqin and Kessler, Roland and Lube, Gert (2010) Enhancement of an Industrial Finite-Volume Code for Large-Eddy-Type Simulation of Incompressible High-Reynolds Number Flow Using Near-Wall Modelling. Computer Methods in Applied Mechanics and Engineering, 199 (13-16), pp. 890-902. Elsevier. doi: 10.1016/j.cma.2009.01.005. Volltext nicht frei.

Krimmelbein, Normann and Krumbein, Andreas (2011) Automatic Transition Prediction for Three-Dimensional Configurations with Focus on Industrial Application. Journal of Aircraft, 48 (6), pp. 1878-1887. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.56700. ISSN 0021-8669. Volltext nicht frei.

Krimmelbein, Normann (2010) Automatic Transition Prediction for Three-Dimensional Configurations with Focus on Industrial Application. 40th Fluid Dynamics Conference and Exhibit, 28 June - 1 July 2010, Chicago, Illinois, USA. Volltext nicht frei.

Krimmelbein, Normann (2011) Automatic Transition Prediction with the eN-Method for Three-Dimensional, Industrially Relevant Configurations. In: CD-ROM Proceedings. ONERA, Centre de Toulouse. 11th ONERA-DLR Aerospace Symposium - ODAS 2006, 09.-11. Feb. 2011, Toulouse, Frankreich. Volltext nicht frei.

Krimmelbein, Normann and Krumbein, Andreas (2010) Automatic Transition Prediction for Three-Dimensional Configurations with Focus on Industrial Application. 40th Fluid Dynamics Conference and Exhibit, 28 June - 1 July 2010, Chicago, Illinois, USA.

Krimmelbein, Normann and Krumbein, Andreas and Togiti, Vamshi (2010) Industrialization of Automatic Transition Prediction for Three-Dimensional Configurations with the eN-Method. 17. DGLR-Fach-Symposium der STAB, 09. Nov. - 10. Nov. 2010, Berlin, Germany. Volltext nicht frei.

Kroll, Norbert (2006) ADIGMA - A EUROPEAN PROJECT ON THE DEVELOPMENT OF ADAPTIVE HIGHER ORDER VARIATIONAL METHODS FOR AEROSPACE APPLICATIONS. ECCOMAS CFD 2006, 2006-09-05 - 2006-09-08, Egmond aan Zee, The Netherlands.

Kroll, Norbert (2009) ADIGMA - A European Project on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications. ECCOMAS Conference 2009, 28.03. - 31.03.2009, Trento, Italien. (Unpublished) Volltext nicht online.

Kroll, Norbert (2009) Numerical Simulation Capabilities for Aircraft Design - Recent Development Activities at DLR. 21st Century Challenges in Computational Engineering and Science, 19. - 21. Nov. 2009, Princeton, USA. (Unpublished) Volltext nicht online.

Kroll, Norbert (2009) ADIGMA - A European Project on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications. 47th AIAA Aerospace Sciences Meeting, 05. - 08. Jan. 2009, Orlando, USA. (Unpublished) Volltext nicht online.

Kroll, Norbert (2010) Impact on High Performance Computing on Aircraft Design. Summer School "High Performance Computing", 04. Okt. 2010, Berlin. Volltext nicht online.

Kroll, Norbert (2010) Numerical Simulation Capabilities for Aircraft Design - Status and Expectations. UKAA Consortium Conference, 07. April 2010, Loughborough, United Kingdom. Volltext nicht online.

Kroll, Norbert (2010) ADIGMA - A European Project on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications - Specific Target Research Project. ECCOMAS Conference 2010, 14.-17. Juni 2010, Lissabon, Portugal. Volltext nicht online.

Kroll, Norbert and Becker, Klaus (2009) Numerical Simulation Capabilities for Aeronautics - A Major Concentrated Activity to Address the Challenge. ISC '09 International Supercomputing Conference, 23. - 26. Jun. 2009, Hamburg, Deutschland. (Unpublished) Volltext nicht online.

Kroll, Norbert and Becker, Klaus and Rieger, Herbert and Thiele, Frank (2009) MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107. Springer-Verlag Berlin, Heidelberg. doi: 10.1007/978-3-642-04093-1. ISBN 978-3-642-04092-4. ISSN 1612-2909. Volltext nicht online.

Kroll, Norbert and Bieler, Heribert and Deconinck, Herman and Couaillier, Vincent and van der Ven, Harmen and Sorensen, Kaare (2010) ADIGMA-A European Project on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications. Springer-Verlag Berlin, Heidelberg. ISBN 978-3-642-03706-1. ISSN 1612-2909. Volltext nicht online.

Kroll, Norbert and Gauger, Nicolas and Brezillon, Joel and Dwight, Richard and Fazzolari, Antonio and Vollmer, Daniel and Becker, Klaus and Barnewitz, Holger and Schulz, Volker and Hazra, Subhendu (2005) Flow Simulation and Shape Optimization For Aircraft Design. Journal of Computational and Applied Mathematics, 203, pp. 397-411. Volltext nicht online.

Kroll, Norbert and Cambier, Laurent (2006) MIRACLE - A Joint DLR/ONERA Effort on Harmonization and Development of Industrial and Research Aerodynamic Computational Environment. 7th ONERA-DLR Aerospace Symposium, ODAS 2006, 2006-10-04 - 2006-10-06, Toulouse, France.

Krumbein, Andreas (1999) Laminar-turbulente Transitionsvorgabe und Transitionsvorhersage im DLR Navier-Stokes-Löser FLOWer unter Verwendung ingenieurmäßiger Methoden. Vortrag. 9. AG STAB-Workshop, 1999-09-11 - 1999-10-11, Göttingen (Deutschland). Volltext nicht online.

Krumbein, Andreas (2005) Automatic Transition Prediction and Application to 3D Wing Configurations – Current Status of Development and Validation. 12. AG STAB-Workshop, 2006-08-11 - 2006-09-11, Göttingen (Deutschland).

Krumbein, Andreas (2007) Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code. Presentation at the Final Meeting of the DLR/ONERA Common Research Project MIRACLE. [Other]

Krumbein, Andreas and Krimmelbein, Normann (2010) Automatic Transition Prediction for Unsteady Airfoil Flows Using the eN-Method. Geschäftsstelle der AG STAB, c/o DLR, Bunsenstr. 10, 37073 Göttingen. 17. DGLR-Fach-Symposium der STAB, 09. - 10. Nov. 2010, Berlin, Deutschland.

Krumbein, Andreas and Krimmelbein, Normann and Seyfert, Cornelia (2011) Automatic Transition Prediction in Unsteady Airfoil Flows Using an Unstructured CFD Code. 29th AIAA Applied Aerodynamics Conference, 27. - 30. June 2011, Honolulu, Hawaii, USA. Volltext nicht frei.

Krumbein, Andreas (2004) Automatic Transition Prediction and Application to 2-dimensio­nal Airfoil Configurations using the DLR TAU code. DLR-Interner Bericht. DLR-IB 124-2004/13. (Unpublished) Volltext nicht frei.

Krumbein, Andreas (2004) Automatic Transition Prediction and Application to High-Lift Multi-Ele­ment Configurations. DLR-Interner Bericht. DLR-IB 124-2004/12. (Unpublished) Volltext nicht frei.

Krumbein, Andreas (2003) Application of the DLR Reynolds-averaged Navier-Stokes Solver FLOWer to the HiReTT Wing-Body Geometry with Control Devices at High Reynolds Numbers. Project Report. HIRETT/TR/DLR/AK/05112003/1. (Unpublished) Volltext nicht frei.

Krumbein, Andreas (2005) Automatic Transition Prediction for High-Lift Systems Using a Hybrid Flow Solver. Journal of Aircraft, Vol. 4 (No. 5), pp. 1150-1164. AIAA. Volltext nicht frei.

Krumbein, Andreas (2005) Automatic Transition Prediction and Application to High-Lift Multi-Element Configurations. Journal of Aircraft, Vol. 4 (No. 5), pp. 1362-1366. AIAA. Volltext nicht frei.

Krumbein, Andreas (2005) Navier-Stokes Airfoil Computations with Automatic Transition Prediction using the DLR TAU code – A Sensitivity Study. erschienen: 2006, S. 192-199. New Results in Numerical and Eperimental Fluid Mechanics V, in: Notes on Numerical Fluid Mechanics and Multidisciplinary Design - Vol. 92, Springer Verlag. ISBN ISBN-10 3-540-33286-3, ISBN-13 978-3-540-33286-2.

Krumbein, Andreas (2006) Automatic Transition Prediction and Application to 3D Wing Configurations. 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006-01-09 - 2006-01-12, Reno, NV (USA). Volltext nicht frei.

Krumbein, Andreas (2006) RANS Computational Results on LSWT cases for TC214 without and with Prescribed and Predicted Transition. Project Report. D1.2.2-4. 111 S. (Unpublished) Volltext nicht frei.

Krumbein, Andreas (2006) Automatic Transition Prediction and Application to 3D High-Lift Configurations. AIAA 24th Applied Aerodynamics Conference. AIAA 24th Applied Aerodynamics Conference, 2006-06-05 - 2006-06-08, San Francisco, CA (USA). Volltext nicht frei.

Krumbein, Andreas (2006) eN Transition Prediction for 3D Wing Configurations using Database Methods and a local, linear Stability Code. ONERA, Centre de Toulouse. 7th ONERA-DLR Aerospace Symposium - ODAS 2006, 2006-10-04 - 2006-10-07, Toulouse, Frankreich.

Krumbein, Andreas (2007) Automatic Transition Prediction and Application to Three-Dimensional Wing Configurations. Journal of Aircraft, Vol. 4 (No. 1), pp. 119-133. American Institute of Aeronautics and Astronautics. doi: 10.2514/1.22254. Volltext nicht frei.

Krumbein, Andreas (2007) Improved Transition Prediction in FLOWer. Project Report. Volltext nicht frei.

Krumbein, Andreas (2007) Automatic Transition Prediction and Application to Three-Dimensional High-Lift Configurations. Journal of Aircraft, Vol. 4 (No. 3), pp. 918-926. American Institute of Aeronautics and Astronautics. doi: 10.2514/1.25528. Volltext nicht frei.

Krumbein, Andreas (2000) Laminar-turbulente Transitionsvorgabe im the DLR Navier-Stokes-Löser FLOWer (Laminar turbulent transition specification in the DLR Navier-Stokes solver FLOWer). ZAMM - Zeitschrift für angewandte Mathematik und Mechanik, Volume (Supple), [477]-[478]. WILEY-VCH Verlag GmbH, Postfach 101161, 69451 Berlin.

Krumbein, Andreas (2008) eN transition prediction for 3D wing configurations using database methods and a local, linear stability code. Aerospace Science and Technology, Vol. 1, pp. 592-598. Elsevier. doi: 10.1016/j.ast.2008.01.005. Volltext nicht frei.

Krumbein, Andreas and Krimmelbein, Normann (2007) Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code. Notes on Numerical Fluid Mechanics and Multidisciplinary Design • Volume 96, New Results in Numerical and Experimental Fluid Mechanics VI, Seiten 210-218. Springer Verlag, Berlin-Heidelberg-New York. ISBN 3-540-74458-4.

Krumbein, Andreas and Krimmelbein, Normann (2008) Automatic Transition Prediction for High-Lift Configurations using a Hybrid CFD Code. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, NV (USA). Volltext nicht frei.

Krumbein, Andreas and Krimmelbein, Normann (2008) Application of the Automatic Transition Prediction Functionality of the DLR TAU Code to 3D Aircraft Configurations. Joint Symposium of DFG PAK 136 and DLR-Airbus C²A²S²E - Simulation of Wing and Nacelle Stall, 2008-06-18 - 2008-06-19, Braunschweig, Niedersachsen (Deutschland).

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2007) Application of a Hybrid Navier-Stokes Solver with Automatic Transition Prediction. American Institute of Aeronautics and Astronautics,. AIAA 25th Applied Aerodynamics Conference, [2007-06-25 - 2007-06-28], AIAA-2007-4284, Miami, Florida, U.S.A..

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2007) Automatic Transition Prediction in the DLR TAU Code - Current Status of Development and Validation. 13. STAB-Workshop, 2007-14-11 - 2007-15-11, Göttingen (Deutschland).

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2008) Automatic Transition Prediction for Three-Dimensional Aircraft Configurations using the DLR TAU Code. In: eingereicht zur Veröffentlichung (DOI: 1), pp. 101-108. Springer Verlag, Berlin-Heidelberg-New York. 16. DGLR-Fach-Symposium der STAB, [2008-11-03 - 2008-11-04], [Aachen, Germany]. ISBN ISBN: 978-3-642-14242-0.

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2009) Automatic Transition Prediction in a Hybrid Flow Solver, Part 1: Methodology and Sensitivities. Journal of Aircraft, 46 (4, I), pp. 1176-1190. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.39736. ISSN 0021-8669. Volltext nicht frei.

Krumbein, Andreas and Krimmelbein, Normann and Schrauf, Géza (2009) Automatic Transition Prediction in a Hybrid Flow Solver, Part 2: Practical Application. Journal of Aircraft, 46 (4, II), pp. 1191-1199. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.39738. ISSN 0021-8669. Volltext nicht frei.

Krumbein, Andreas and Radespiel, Rolf (2011) RANS modeling of transition in external flows I + II. ERCOFTAC - European Research Community on Flow, Turbulence and Combustion. [Other] Volltext nicht frei.

Krumbein, Andreas and Rakowitz, Mark (2003) Application of the DLR Reynolds-averaged Na­vier-Stokes Solver FLOWer to the Clean HiReTT Wing-Body Geometry at High Reynolds Numbers. Project Report. HIRETT/TR/DLR/AK/03112003/1. (Unpublished) Volltext nicht frei.

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Lambert, Markus and Kessler, Roland (2010) Radiation Heat Transfer in Mixed Convection Flows. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112. Springer Verlag, Berlin Heidelberg. pp. 563-570. doi: 10.1007/978-3-642-14243-7_69. ISBN 978-3-642-14242-0. ISSN 1612-2909. Volltext nicht online.

Lambert, Markus and Kessler, Roland (2008) Radiation Heat Transfer in Mixed Convection Flows. 16th DGLR Symposium of STAB, 2008-11-03 - 2008-11-04, Aachen. Volltext nicht frei.

Lambert, Markus and Kessler, Roland and Di Domenico, Massimiliano and Noll, Berthold, Erich (2011) The DLR THETA code, the incompressible brother of TAU, an overview. TAU User Meeting 2011, 18. - 19. Oct. 2011, Braunschweig, Germany.

Langer, Stefan (2011) Application of first order implicit methods for the simulation of stationary flow problems on unstructured meshes. STAB Workshop 2011, 09.11.2011 - 10.11.2011, Göttingen, Deutschland. (Unpublished) Volltext nicht online.

Langer, Stefan and Li, Dian (2011) Application of point implicit Runge–Kutta methods to inviscid and laminar flow problems using AUSM and AUSM+ upwinding. International Journal of Computational Fluid Dynamics, 25 (5), pp. 255-269. Taylor & Francis. doi: 10.1080/10618562.2011.590801. ISSN 1061-8562. Volltext nicht online.

Le Chuiton, Frederic (2003) Experience with the implementation of the Baldwin-Lomax turbulence model in FLOWer. DLR-Interner Bericht. DLR-IB 124-2003/26. 28 S. Volltext nicht online.

Le Chuiton, Frederic (2004) FLOWer/elsA comparison: scalar artificial dissipation and Martinelli correction. DLR-Interner Bericht. DLR IB 124-2004/3. 11 S. Volltext nicht online.

Le Chuiton, Frederic (2003) Actuator disc modelling for helicopter rotors. DLR-Interner Bericht. DLR-IB 124-2003/22. 27 S. Volltext nicht online.

Le Chuiton, Frederic (2005) Chimera Simulation of a Complete Helicopter with Rotors as Actuator Discs. Springer. (In Press) Volltext nicht online.

Le Chuiton, Frederic and D'Alascio, A. and Barakos, G. and Steijl, R. and Schwamborn, Dieter and Lüdeke, Heinrich (2008) Computation of the Helicopter Fuselage Wake with the SST, SAS, DES and XLES Models. In: Advances in Hybrid RANS-LES Modelling Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol.: 97. Springer-Verlag Berlin. ISBN 978-3-540-77813-4. Volltext nicht online.

Le Chuiton, Frederic and D'Alascio, A. and Barakos, G. and Steijl, R. and Schwamborn, Dieter and Lüdeke, Heinrich (2007) Computation of the Helicopter Fuselage Wake with the SST, SAS, DES and XLES Models. Numerical Fluid Mechanics and Multidisciplinary Design 2nd Hybrid RANS-LES Symposium, 2007-06-17 - 2007-06-18, Corfu (Griechenland). Volltext nicht frei.

Lee, Jen-Der and Abu-Zurayk, Mohammed and Brezillon, Joel (2009) Inverse design using adjoint approach. In: STAB Mitteilungen. 14. STAB-Workshop, Göttingen. Volltext nicht online.

Leicht, Tobias (2011) DG methods for aerodynamic flows: hp-adaptive meshes with anisotropic element subdivision. 16th Int. Conference on Finite Elements in Flow Problems, 23.-25.03.2011, München. (Unpublished) Volltext nicht online.

Leicht, Tobias and Hartmann, Ralf (2011) Error estimation and hp–adaptive mesh refinement for discontinuous Galerkin methods. In: Advances in Computational Fluid Dynamics, 2. World Scientific Books. pp. 67-94. ISBN 978-981-4313-18-6. Volltext nicht online.

Leicht, Tobias (2006) Anisotropic Mesh Refinement for Discontinuous Galerkin Methods in Aerodynamic Flow Simulations. Diploma, TU Dresden.

Leicht, Tobias (2009) Ein CFD-Verfahren variabler Ordnung auf adaptiven Netzen. STAB Workshop 2009, 11-12 Nov 2009, Göttingen. Volltext nicht frei.

Leicht, Tobias and Hartmann, Ralf (2007) Anisotropic mesh refinement for discontinuous Galerkin methods in two-dimensional aerodynamic flow simulations. Int. J. Numer. Meth. Fluids, 56 (11), pp. 2111-2138. John Wiley & Sons.

Leicht, Tobias and Hartmann, Ralf (2010) Error estimation and anisotropic mesh refinement for 3d laminar aerodynamic flow simulations. Journal of Computational Physics, 229 (19), pp. 7344-7360. Elsevier. doi: 10.1016/j.jcp.2010.06.019. ISSN 0021-9991.

Leicht, Tobias and Hartmann, Ralf (2010) Error estimation and anisotropic mesh refinement for aerodynamic flow simulations. In: Springer. pp. 579-587. ISBN 978-3-540-34287-8.

Li, Chunna and Brezillon, Joël and Görtz, Stefan (2011) A hybrid approach for surrogate-based aerodynamic optimization with constraints. In: EVOLUTIONARY AND DETERMINISTIC METHODS FOR DESIGN, OPTIMIZATION AND CONTROL with Applications Industrial and Societal Problems (Collection of Abstracts). CIMNE, Barcelona, Spain 2011. ECCOMAS Thematic Conference, EUROGEN 2011, 14-16 Sep 2011, Capua, Italy. Volltext nicht frei.

Li, Chunna and Brezillon, Joël and Görtz, Stefan (2011) A framework for surrogate-based aerodynamic optimization. ODAS 2011, 9-11 Feb 2011, Toulouse, France.

Lincke, Anne (2009) Verification and Validation of von Karman Length Scale for Identification of Turbulent Structures. Diploma, DLR-AS. Volltext nicht online.

Lincke, Anne (2010) Verification and Validation of von Karman Length Scale for Identification of Turbulent Structures. Diploma, DLR, AS, Göttingen und Universität Göttingen.

Lube, Gerd and Knopp, Tobias and Gritzki, R. and Rösler, M. and Seifert, J. (2008) Application of domain decomposition methods to indoor air flow simulation. International Journal of Computer Mathematics (85), pp. 1551-1562. Volltext nicht online.

Lube, Gerd and Knopp, Tobias and Rapin, G. and Gritzki, R. and Rösler, M. (2008) Stabilized finite element methods to predict ventilation efficiency and thermal comfort in buildings. International Journal for Numerical Methods in Fluids (57), pp. 1269-1290. Volltext nicht online.

Lüdeke, H. and Leicher, S. (2008) Unsteady CFD Analysis of a Delta Wing Fighter Configuration by Delayed Detached Eddy Simulation. In: Advances in Hybrid RANS-LES Modelling, Vol.: . Springer-Verlag Berlin. pp. 202-211. ISBN 978-3-540-77813-4.

Lüdeke, Heinrich (2006) Detached Eddy Simulation of a Delta Wing With Rounded Leading Edge. In: Proceedings of the 7th ONERA DLR Aerospace Symposium, ODAS 2006. 7th ONERA DLR Aerospace Symposium, ODAS 2006, 2006-10-04 - 2006-10-06, Toulouse, France. Volltext nicht frei.

Lüdeke, Heinrich and Calvo, Javier B. and Filimon, Alexander (2006) Fluid Structure Interaction at the ARIANE-5 Nozzle section by Advanced Turbulence Models. In: Proceedings of the European Conference on Computational Fluid Dynamics. European Conference on Computational Fluid Dynamics, 2006-09-05 - 2006-09-08, Egmond aan Zee, The Netherlands. Volltext nicht frei.

Lüdeke, Heinrich and Togiti, Vamshi (2006) Detached Eddy Simulation of Supersonic Shear Layer Wake Flows. In: Int. Conference on Boundary and Interior Layers. Int. Conference on Boundary and Interior Layers, 2006-07-24 - 2006-07-28, Göttingen, Germany.

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Mayer, Ursula and Dwight, Richard (2006) A Fourth Order Semi-Implicit Runge-Kutta Method for the Compressible Euler Equations. DLR-Interner Bericht. DLR-IB 124-2007/3. Master's. TU Munich.

Meinel, Michael (2008) FlowSimulator: A Python-controlled framework to unify massive parallel, multi-discipline CFD workflows. EuroPython 2008, 7.-9. Jul. 2009, Vilnius, Litauen. Volltext nicht frei.

Meinel, Michael (2009) FlowSimulator: A Python-controlled Approach to Unify Future CFD Simulation Workflows. EuroSciPy 2009, 25.-26. Jul. 2009, Leipzig, Deutschland. Volltext nicht frei.

Meinel, Michael and Einarsson, Gunnar O. (2010) The FlowSimulator framework for massively parallel CFD applications. In: PARA 2010. PARA2010, 6.-9. Juni 2010, Reykjavik, Island.

Michler, Andreas and Heinrich, Ralf (2010) Numerical Simulation of the Elastic and Trimmed Aircraft. In: New Results in Numerical and Experimental Fluid Mechanics VII, Vol. 112, pp. 109-116. Springer. 16. STAB-Symposium, November 2008, Aachen. ISBN ISBN 978-3-642-14242-0. ISSN ISSN 1612-2909. Volltext nicht online.

Michler, Andreas K. (2010) Aircraft Control Surface Deflection using RBF-based Mesh Deformation. In: Proceedings of the 5th European Conference on Computational Fluid Dynamics, Eccomas CFD 2010. V European Conference on Computational Fluid Dynamics Eccomas CFD 2010, 14-17 June 2010, Lisbon, Portugal. Volltext nicht online.

Michler, Andreas K. (2011) Aircraft control surface deflection using RBF-based mesh deformation. International Journal for Numerical Methods in Engineering, 88 (10), pp. 986-1007. Wiley. doi: 10.1002/nme.3208. Volltext nicht online.

Mifsud, Michael and Zimmermann, Ralf and Sippli, Jan and Görtz, S. (2011) A POD-based reduced order modeling approach for the efficient computation of high-lift aerodynamics. International Conference on Evolutionary and Deterministic Methods for Design, Optimization and Control with Applications to Industrial and Societal Problems (Eurogen 2011), 14-16 Sep 2011, Capua, Italy. Volltext nicht online.

Moens, Frédéric and Perraud, Jean and Krumbein, Andreas and Toulorge, Thomas and Iannelli, Pierluigi and Eliasson, Peter and Hanifi, Ardeshir (2007) Transition Prediction and Impact on 3D High-Lift Wing Configuration. American Institute of Aeronautics and Astronautics,. 25th AIAA Applied Aerodynamics Conference, [2007-06-25 - 2007-06-28], AIAA-2007-4302, Miami, Florida, U.S.A.. Volltext nicht frei.

Moens, Frédéric and Perraud, Jean and Krumbein, Andreas and Toulorge, Thomas and Iannelli, Pierluigi and Eliasson, Peter and Hanifi, Ardeshir (2008) Transition Prediction and Impact on a Three-Dimensional High-Lift-Wing Configuration. Journal of Aircraft, Vol. 4 (No. 5), [1751]-[1766]. American Institute of Aeronautics and Astronautics. doi: 10.2514/1.36238. Volltext nicht frei.

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Nigro, A. and De Bartolo, C. and Hartmann, Ralf and Bassi, F. (2010) Discontinuous Galerkin solution of preconditioned Euler equations for very low Mach number flows. International Journal for Numerical Methods in Fluids, 63 (4), pp. 449-467. Wiley. doi: 10.1002/fld.2083. ISSN 0271-2091.

Nigro, Alessandra (2008) Discontinuous Galerkin Methods for inviscid low Mach number flows. DLR-Interner Bericht. DLR-IB 124-2008/1. Dissertation. University of Calabria. 103 S. (In Press)

Nigro, Alessandra and Renda, Salvatore Manuel and De Bartolo, Carmine and Hartmann, Ralf and Bassi, Francesco (2011) A discontinuous Galerkin method for laminar low Mach number flows. 66th National Congress ATI, 5-9 Sept 2011, Rende, Italy.

Noll, Berthold and Meier, Wolfgang and Frank, Peter and Kessler, Roland and Aigner, Manfred (2006) Numerical Analysis of Combustion Systems- Ergebnisse des Projekts NACOS 2002-2005. DLR-Interner Bericht. Volltext nicht online.

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Pahlke, Klausdieter (2002) Application of the Standard Aeronautical CFD Method FLOWer to Trains Passing on Open Track. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 79. Springer. pp. 160-169. ISBN 3-540-43316-3. Volltext nicht online.

Pahlke, Klausdieter and Costes, Michel and D'Alascio, Alessandro and Castellin, Christophe and Altmikus, Andree (2006) THE FRENCH-GERMAN HELICOPTER CFD-PROJECT CHANCE. In: Deutscher Luft- und Raumfahrtkongress 2006 (86), pp. 173-182. Deutscher Luft- und Raumfahrtkongress 2006, 2006-11-07, Braunschweig. ISSN 0700-4083. Volltext nicht online.

Pahlke, Klausdieter and Costes, Michel and D'Alascio, Alessandro and Castellin, Christophe and Altmikus, Andree (2006) CHANCE: A FRENCH-GERMAN HELICOPTER CFD-PROJECT. In: ODAS 2006. ODAS 2006, 2006-10-04, Toulouse, Frankreich.

Prill, F and Lukacova-Medvidova, M and Hartmann, R (2009) Smoothed Aggregation Multigrid for the Discontinuous Galerkin Method. SIAM Journal on Scientific Computing, 31, pp. 3503-3528. SIAM - Society for Industrial and Applied Mathematics. ISSN 0196-5204. Volltext nicht online.

Prill, F and Lukacova-Medvidova, M and Hartmann, R (2009) A Multilevel Discontinuous Galerkin Method for the Compressible Navier-Stokes Equations. Algoritmy 2009. 18th conference on scientific computing, March 15-20 2009, Slovakia. Volltext nicht online.

Probst, Axel and René, Cécora and Rolf, Radespiel (2011) Near-wall Reynolds stress modelling for RANS and hybrid RANS/LES methods. TAU User Meeting 2011, 18. - 19. Okt. 2011, Braunschweig. Volltext nicht frei.

Probst, Axel and Radespiel, Rolf and Knopp, Tobias (2011) Detached-Eddy Simulation of Aerodynamic Flows Using a Reynolds-Stress Background Model and Algebraic RANS/LES Sensors. 20th AIAA Computational Fluid Dynamics Conference, 27. - 30. Jun. 2011, Honolulu, Hawaii, USA. Volltext nicht frei.

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Raichle, Axel and Stefan, Melber-Wilkending and Himisch, Jan (2006) A new Actuator Disk Model for the TAU Code and application to a sailplane with a folding engine. STAB-Symposium 2006, 2006-11-29 - 2006-12-01, Darmstadt. (Submitted) Volltext nicht online.

Reimer, Lars (2004) Anwendung eines Transitions-/Turbulenzmodells zur numerischen Simulation von Strömungen mit Transition – Implementierung und Validierung der Methode unter Verwendung des Strömungslösers FLOWer. DLR-Interner Bericht. DLR-IB 124-2004/15.

Reuß, Silvia and Knopp, Tobias and Schwamborn, Dieter (2011) Hybrid RANS/LES simulations of a three-element airfoil. Fourth Symposium on Hybrid RANS-LES Methods, 28-30 Sep 2011, China, Peking. Volltext nicht frei.

Reuß, Silvia and Knopp, Tobias and Schwamborn, Dieter (2010) Best Practice for starting a detached eddy simulation on the F15 geometry. STAB 2010, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.

Richter, Kai and Le Pape, Arnaud and Knopp, Tobias and Costes, Michel and Gleize, Vincent and Gardner, Anthony Donald (2011) Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods. Journal of the American Helicopter Society, 56 (04), 042001-042012. American Helicopter Society. doi: 10.4050/JAHS.56.042007. ISSN 0002-8711. Volltext nicht online.

Roosenboom, Eric and Schade, N. and Acisu, I. and Schröder, Andreas (2009) Experimental and Numerical Investigation of the Near-Field Wake behind a Transport Aircraft with an Open Ramp. 4th Symposium on Integrating CFD and Experiments in Aerodynamics, 14-16 September 2009, Sint-Genesius-Rode, Belgium. Volltext nicht online.

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Schröder, Simon and Knopp, Tobias (2010) Turbulence Model Assessment Database : Concept and implementation using WebDAV and DataFinder. DLR-Interner Bericht. DLR-IB 224-2010 A 45. 35 S. Volltext nicht frei.

Schwamborn, Dieter (2006) DLR F6. In: NNFM Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 94. Springer Verlag. pp. 400-404. ISBN 3-540-28786-8. Volltext nicht online.

Schwamborn, Dieter and Gerhold, Thomas and Heinrich, Ralf (2006) THE DLR TAU-CODE: RECENT APPLICATIONS IN RESEARCH AND INDUSTRY. ECCOMAS CFD 2006 CONFERENCE, 2006-04-09 - 2006-08-09, Netherlands. Volltext nicht online.

Schwamborn, Dieter and Strelets, Mikhail (2011) ATAAC – An EU-Project Dedicated to Hybrid RANS/LES Methods. 4th Symposium on Hybrid RANS-LES Methods, 28. - 30. Sep. 2011, Beijing, China. Volltext nicht frei.

Schwamborn, Dieter and Voß, Ralph and Mack, Andreas and Pahlke, Klausdieter and Schütte, Andreas (2004) Recent and future DLR projects on multidisciplinary simulation and validation. Promuval - Multidisciplinary Modelling, Simulation and Validation in Aeronautics, Barcelona, Spain, 28-29 June 2004, 2004-06-28 - 2004-06-29, Barcelona, Spain. Volltext nicht online.

Schwamborn, Dieter and Gardner, Anthony and von Geyr, Heiko and Krumbein, Andreas and Lüdeke, Heinrich and Stürmer, Arne (2008) Development of the TAU-Code for aerospace applications. 50th NAL International Conference on Aerospace Science and Technology, 2008-06-26 - 2008-06-28, Bangalore (India).

Schwarz, Thorsten (2000) Development of a Wall Treatment for Navier-Stokes Computations using the Overset-Grid Technique. 26th European Rotorcraft Forum, 2000-09-26 - 2000-09-29, The Hague, The Netherlands. Volltext nicht online.

Schwarz, Thorsten (2002) Enhancement of a Navier-Stokes Flow Solver for Patched Grids with Non-Coincident Grid Nodes. New Results in Numerical and Experimental Fluid Dynamics III, 77, pp. 312-319. Springer Verlag , Berlin, Heidelberg, New York. Volltext nicht online.

Schwarz, Thorsten (2005) The Overlapping Grid Technique for the Time Accurate Simulation of Rotorcraft Flows. 31st European Rotorcraft Forum, 2005-09-13 - 2005-09-15, Florence, Italy. Volltext nicht online.

Schwarz, Thorsten (2009) An Interpolation Method Maintaining the Wall Distance for Structured and Unstructured Overset Grids. In: Proceedings of the CEAS 2009 conference. CEAS 2009 European Air and Space Conference, 26. - 29 October 2009, Manchester, UK. Volltext nicht frei.

Schwarz, Thorsten and Khier, Walid and Raddatz, Jochen (2006) Simulation of the Unsteady Flow Field around a Complete Helicopter with a Structured RANS Solver. In: High Performance Computing on Vector Systems, pp. 125-137. Springer Verlag , Berlin, Heidelberg, New York. Second Teraflop Workbench Project Workshop, 2005-03, Stuttgart, Germany. ISBN 3-540-29124-5. Volltext nicht online.

Schwarz, Thorsten and Khier, Walid and Raddatz, Jochen (2006) Simulation of the Unsteady Flow around the Complete BO-105 Wind Tunnel Model. 7th ONERA-DLR Aerospace Symposium 2006 (ODAS 2006), 2006-10-04 - 2006-10-06, Toulouse, France. Volltext nicht frei.

Schwarz, Thorsten and Pahlke, Klausdieter (2010) The GOAHEAD project – overview and selected results. 36th European Rotorcraft Forum, 7.-9. Sep. 2010, Paris, Frankreich. Volltext nicht frei.

Schwarz, Thorsten (2005) Ein blockstrukturiertes Verfahren zur Simulation der Umströmung komplexer Konfigurationen. DLR-Forschungsbericht. DLR-Forschungsbericht 2005-20. Dissertation. TU Braunschweig. 122 S.

Schwarz, Thorsten (2007) RANS Simulations with One and Six Degrees of Freedom Rigid Body Motions. In: New Results in Numerical and Experimental Fluid Mechanics VI, 96, pp. 178-185. Springer-Verlag , Berlin, Heidelberg. 15 th STAB/DGLR Symposium, 2006-11-29 2006-12-01, Darmstadt (Germany). ISBN 3-540-74458-4. Volltext nicht frei.

Schwöppe, Axel and Heinrich, Ralf (2006) Flow Solver Algorithms and Data Structures for TAUijk. DLR-Interner Bericht. DLR-IB 124-2006/006. 39 S. Volltext nicht frei.

Schütte, Andreas and Bruse, Martin and Henne, Ulrich (2001) Experimentelle Untersuchungen an Vielflächen-Doppeldelta-Konfigurationen im DNW-TWG. DGLR Luft-und Raumfahrtkongress, 2001-09-17 - 2001-09-20, Hamburg (Germany). Volltext nicht online.

Schütte, Andreas and Konrath, Robert and Lüdeke, Heinrich (2007) Numerical studies of the vortical flow around delta wing with rounded leading edges in comparison to experimental data within the Vortex Flow Experiment (VFE-2). Joint EWA and DESider Workshop on Validation of Numerical Methods by Experiments in Aerodynamics, 2006-06-13 - 2006-06-14, Stockholm. Volltext nicht online.

Schütte, Andreas and Einarsson, Gunnar and Raichle, Axel and Schöning, Britta and Orlt, Matthias and Neumann, Jens and Arnold, Jürgen and Mönnich, Wulf and Forkert, Thomas (2007) Numerical Simulation of Maneuvering Aircraft by Aerodynamic, Flight Mechanics and Structural Mechanics Coupling. AIAA. 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007-01-08 - 200/-01-11, Reno, Nevada, USA.

Schütte, Andreas and Konrath, Robert and Lüdeke, Heinrich (2005) Numerische und experimentelle Untersuchung der Wirbelströmung um Deltaflügel mit runden Vorderkanten. 12. STAB Workshop, 2005-11-08 - 2005-11-11, Göttingen (Deutschland). Volltext nicht online.

Schütte, Andreas and Rein, Martin and Höhler, Gebhard (2007) Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration. Third Symposium on Integration of CFD and Experiments in Aerodynamics, 2007-06-20 - 2007-06-21, United States Air Force Academy, Colorado, USA. Volltext nicht frei.

Seyfert, Cornelia (2011) Application of a Transition Transport Model to Industrially Relevant Aerodynamic Configurations. ODAS 2011, 08. - 10. Feb. 2011, Toulouse, France.

Seyfert, Cornelia and Krumbein, Andreas (2010) Evaluation of a Correlation-Based Transition Model and Comparison with the eN-method. 40th Fluid Dynamics Conference and Exhibit, 28.06. - 01.07.2010, Chicago, USA. ISBN 978-1-60086-745-3 . Volltext nicht frei.

Seyfert, Cornelia and Krumbein, Andreas (2010) Comparison of a Local Correlation-Based Transition Transport Model with a eN-method for Transition Prediction. 17. DGLR-Fach-Symposium der STAB, 09.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht frei.

Seyfert, Cornelia and Schwamborn, Dieter and Kessler, Roland (2010) TAU und THETA - CFD in Verkehr, Energie, Luft- und Raumfahrt. ProcessNet Jahrestreffen, Fachausschuss CFD, 08.-10.03.2010, Hamburg, Deutschland. Volltext nicht frei.

Sides, Jacques and Pahlke, Klausdieter and Costes, Michel (2001) Numerical Simulation of Flows around Helicopters at DLR and ONERA. Aerospace Science and Technology, 5, pp. 35-53. ISSN 1270-9638. Volltext nicht online.

Simmendinger, Christian and Jägersküpper, Jens and Machado, Rui and Lojewski, Carsten (2011) A PGAS-based Implementation for the Unstructured CFD Solver TAU. 5th Conference on Partitioned Global Address Space Programming Models, 15. - 18. Okt. 2011, Tremont House, Galveston Island, Texas, USA. Volltext nicht online.

Spiering, Frank and Heinrich, Ralf and Keye, Stefan (2010) Entwicklung einer parallelen Kopplungsumgebung und Anwendung bei einem Windkanalmodell unter hoher aerodynamischer Last. DGLR-Fach-Symposium der STAB 2010, 09.-10. Nov. 2010 , Berlin. Volltext nicht online.

Splettstößer, Wolf R. and Prieur, Jean and Pahlke, Klausdieter and Schultz, K.-J. and van der Wall, Berend G. and Delrieux, Yves and Gardarein, Patrick and Geoffroy, P. and Leconte, Philippe (1997) Main Phase of the ERATO Cooperation on Aeroacoustic Rotor Optimization. DLR-Interner Bericht. DLR-IB 129-97/10, ONERA TRS 131/5094 PY. 67 S. (Unpublished) Volltext nicht online.

Stock, H. W. and Krumbein, Andreas (2003) 2D High-Lift RANS Computations with e<sup>N</sup> Transi­tion Predic­tion – A310 Take-Off and Landing Configuration. Project Report. HiAer Report D1.3-2. (Unpublished) Volltext nicht frei.

Stock, H. W. and Wild, Jochen and Krumbein, Andreas (2004) Computation of an Infinite Swept High Lift System at Four Angles of Attack – RANS Computations Coupled to the 2 N-Factor e<sup>N</sup> Transition Prediction. Project Report. HiAer Report D1.4-2. (Unpublished) Volltext nicht frei.

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Vollmer, Daniel (2007) Using the Adjoint Formulation for Target Functional-Based Mesh-Adaptation. DLR-Interner Bericht. DLR-IB 124-2007/1. 22 S.

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Weinman, Keith (2002) Turbulence Model Implementation in TAU. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 89. Springer Verlag. pp. 117-123. ISBN 3-540-24383-6. ISSN 1612-2909. Volltext nicht online.

Weinman, Keith (2006) NACA0012 beyond Stall. In: NNFM Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 94. Springer Verlag. pp. 233-246. ISBN 3-540-28786-8. Volltext nicht online.

Weinman, Keith and van der Ven, H. and Mockett, C.R. and Knopp, T.A. and Kok, J.C. and Perrin, R.T.E and Thiele, F.H. (2006) A study of grid convergence Issues for the simulation of the massively separated flow around a stalled airfoll using DES and related methods. ECCOMAS CFD 2006 Conference, 2006-04-09 - 2006-08-09, Netherlands. Volltext nicht online.

Widhalm, Markus and Arno, Ronzheimer and Martin, Hepperle (2007) Comparison between Gradient-free and Adjoint Based Aerodynamic Optimization of a Flying Wing Transport Aircraft in the Preliminary Design. American Institute of Aeronautics and Astronautics. AIAA 25th Applied Aerodynamics Conference, [2007-06-25 - 2007-06-28], AIAA Miami 4060, Miami, Florida, U.S.A..

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Widhalm, Markus and Schuette, Andreas and Alrutz, Thomas and Orlt, Matthias (2007) Improvement of the Automatic Grid Adaptation for Vortex Dominated Flows using Advanced Vortex Indicators with the DLR-TAU Code. Springer. STAB 2006, Darmstadt.

Wild, Jochen and Mertins, Ralf and Quagliarella, Domenico and Brezillon, Joel and Quest, Jürgen and Amoignon, Olivier and Moens, Frederic (2005) Applying numerical optimization to realistic high-lift design of transport aircraft – an overview of the aerodynamic design optimisation investigations within the EUROLIFT II project. In: Proceedings of the Sixth Conference on Evolutionary and Deterministic Mehtods for Design, Optimization and Control with Applications to Indutsrial and Societal Problems. TU München. EUROGEN 2005, 2005-09-12 2005-09-14, München, BY (D). ISBN 3-00-017534-2. Volltext nicht online.

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Wilke, Gunther (2011) Aerodynamische Optimierung von Hubschrauberrotoren durch Nutzung von numerischen Methoden unterschiedlicher Endringtiefe. Strömungsmechanische Arbeitsgemeinschaft 2011, DLR, Göttingen, Germany.

Wokoeck, Ralf and Grote, Arne and Krimmelbein, Normann and Ortmanns, Jens and Radespiel, Rolf and Krumbein, Andreas (2006) RANS Simulation and Experiments on the Stall Behaviour of a Tailplane Airfoil. erschienen: 2006, S. 208. New Results in Numerical and Eperimental Fluid Mechanics V, in: Notes on Numerical Fluid Mechanics and Multidisciplinary Design - Vol. 92, Springer Verlag. ISBN ISBN-10 3-540-33286-3, ISBN-13 978-3-540-33286-2.

Wokoeck, Ralf and Krimmelbein, Normann and Ortmanns, Jens and Ciobaca, V. and Radespiel, Rolf and Krumbein, Andreas (2006) RANS Simulation and Experiments on the Stall Behaviour of an Airfoil with Laminar Separation Bubbles. 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006-01-09 - 2006-01-12, Reno, NV (USA). Volltext nicht frei.

Wolf, Christoph (2011) A Chimera Simulation Method and Detached Eddy Simulation for Vortex-Airfoil Interactions. DLR-Interner Bericht. DLR-IB 224-2011 A 50. Dissertation. Georg-August-Universität Göttingen. 181 S. Volltext nicht online.

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Yuan, Weixing and Mamou, Mahmoud and Xu, Hongyi and Wokoeck, Ralf and Ortmanns, Jens and Krimmelbein, Normann and Krumbein, Andreas (2004) NRC-HGF Project: RANS Simulation of Reynolds Number Effects on Airfoil Stall Progress Report 2003-2004. Project Report. (Unpublished) Volltext nicht frei.

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Zhang, X. Q. and Knopp, Tobias and Lube, Gerd (2008) Calibration of model and discretization parameters for turbulent channel flow. In: K. Kunisch et al. (eds.), pp. 529-537. Springer Verlag. 7th European Conference on Numerical Mathematics and Advanced Applications, 2007-09-00, Graz ( Austria). Volltext nicht online.

Zhang, Xiaoqin and Knopp, Tobias and Lube, Gert (2008) Calibration of model and discretization parameters for turbulent channel flow. In: Numerical Mathematics and Advanced Applications. Springer. pp. 529-537. ISBN 3540697764. Volltext nicht frei.

Zimmermann, Ralf (2010) An introduction to non-linear POD-based reduced-order models for steady aerodynamics. Oberseminar Numerische Mathematik, Kiel, 11.02.2010, Kiel, Deutschland.

Zimmermann, Ralf (2011) On Efficiently Updating Singular Value Decomposition Based Reduced Order Models. GAMM Workshop Applied and Numerical Linear Algebra with Special Emphasis on Model Reduction, 22.-23. Sep. 2011, Bremen, Deutschland.

Zimmermann, Ralf (2011) Towards best-practice guidelines for POD-based reduced order modeling of transonic flows. CIRA. EUROGEN 2011, 14-16 Sep 2011, Capua, Italy. Volltext nicht online.

Zimmermann, Ralf and Görtz, Stefan (2010) Non-Linear POD-based Reduced Order Models for Steady Turbulent Aerodynamics. RAeS Conference 2010 Applied Aerodynamics: Capabilities And Future Requirements, 27.-28. Juli 2010, Bristol, UK. Volltext nicht online.

Zimmermann, Ralf and Han, Zhong-Hua (2010) Simplified Cross-Correlation Estimation For Multi-Fidelity Surrogate Cokriging Models. Advances and Applications in Mathematical Sciences, 7 (2), pp. 181-202. Mili Publication. ISSN 0974-6803. Volltext nicht online.

Zimmermann, Ralf (2011) A Comprehensive Comparison of Various Algorithms for Efficiently Updating Singular Value Decomposition Based Reduced Order Models. DLR-Interner Bericht. DLR-IB 124-2011/3. DLR Braunschweig. 19 S.

Zimmermann, Ralf and Görtz, Stefan (2010) Non-linear reduced order models for steady aerodynamics. Procedia Computer Science, 1 (1), pp. 165-174. Elsevier. ISSN 1877-0509.