Source: https://elib.dlr.de/view/subjects/as-tf.html
Timestamp: 2019-04-25 11:06:03+00:00

Document:
electronic library - Items where Subject is "Institute of Aerodynamics and Flow Technology > Transport Aircraft"
Items where Subject is "Institute of Aerodynamics and Flow Technology > Transport Aircraft"
Backhaus, Kai and Lüdeke, Heinrich (2016) Validierung des Strömungslösers FLOWer in der 4.-Ordnung Version für direkte numerische Simulationen anhand repräsentativer Vergleichsfälle. DLR-Interner Bericht. DLR-IB-AS-BS-2016-117, 26 S. Volltext nicht online.
Bakunowicz, Jerzy and Boden, Fritz and Groot, Klaus de and Meyer, Jörg Brüne and Meyer, Ralf and Rzucidło, Paweł and Smusz, Robert and Szewczyk, Mariusz and Szumski, Marek (2015) Flow and structure deformation research of a composite glider in flight conditions. 46th Annual SFTE International Symposium, 14. - 17. Sept. 2015, Lancaster, CA, USA. Volltext nicht online.
Belligoli, Zeno and Lüdeke, Heinrich (2014) DNS of Simple Verification Test Cases Using OpenFOAM. DLR-Interner Bericht. DLR-IB 124-2014/2, 40 S. Volltext nicht online.
Benini, E. and Ponza, R. and Iannelli, P. and Strüber, H. and Hrncir, Z. and Moens, F. and Kühn, T. (2012) Multi-Point Shape and Setting Optimization of High-Lift Airfoils in Both Take-Off and Landing Conditions. ECCOMAS 2012 - European Congress on Computational Methods in Applied Sciences and Engineering, 10-14 September 2012, Vienna, Austria. Volltext nicht online.
Bier, N. and Rohlmann, D. and Rudnik, R. (2012) Numerical Maximum Lift Predictions of a Realistic Commercial Aircraft in Landing Configuration. 50th AIAA Aerospace Sciences Meeting, 09 - 12 January 2012, Nashville, TN, USA. Volltext nicht online.
Bier, Niko (2012) Title confidential. DLR-Interner Bericht. IB 124-2012/911. Volltext nicht online.
Bier, Niko (2013) Title confidential. DLR-Interner Bericht. DLR-IB 124-2013/903. Volltext nicht online.
Bier, Niko and Rohlmann, David (2012) Maximum lift predictions of a realistic commercial aircraft in landing configuration. FOR1066 Symposium “Simulation of Wing and Nacelle Stall”, 21.-22. June 2012, Braunschweig, Germany. Volltext nicht online.
Bier, Niko (2014) Title confidential. DLR-Interner Bericht. IB 124-2014/909, 38 S. Volltext nicht online.
Bier, Niko (2015) WIND TUNNEL MEASUREMENTS OF A CUBOID EXTERNAL LOAD MODEL. 41st European Rotorcraft Forum, 1.-4. Sept. 2015, München. Volltext nicht online.
Bier, Niko and Keye, Stefan and Rohlmann, David (2013) Design of a Wind Tunnel Model for Maximum Lift Predictions Based on Flight Test Data. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego. Volltext nicht online.
Bier, Niko and Keye, Stefan and Rohlmann, David (2014) Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data. 4th Joint Symposium of DFG FOR 1066 and DLR C²A²S²E on "Simulation of Wing and Nacelle Stall", 01.-02. Dez. 2014, Braunschweig. Volltext nicht online.
Bier, Niko and Keye, Stefan and Rohlmann, David (2015) Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data. In: Advances in Simulation of Wing and Nacelle Stall Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), 131. Springer. pp. 337-350. ISBN 978-3-319-21126-8. ISSN 1612-2909 Volltext nicht online.
Bier, Niko and Rudnik, Ralf and Keye, Stefan and Rohlmann, David (2016) Advanced Design Approach of a Cryo-Wind-Tunnel-Model For Maximum Lift Prediction. 3rd NPU-DLR Workshop on Aerodynamics, 23.-26. Mai 2016, Xi'An, CHINA. Volltext nicht online.
Bier, Niko and Rudnik, Ralf and Keye, Stefan and Rohlmann, David (2016) Advanced Design Approach of a Cryo-Wind-Tunnel-Model For Maximum Lift Prediction. Deutscher Luft- und Raumfahrtkongress 2016, 13.-15. Sept. 2016, Braunschweig. Volltext nicht online.
Bier, Niko and Rudnik, Ralf and Quest, Jürgen and Rechlin, Alexander (2015) Stall Behavior of the HINVA KH-A320-HA Highlift Model in ETW. 53rd AIAA Aerospace Sciences Meeting, 5.-9. January 2015, Kissimmee (FL), USA. DOI: [10.2514/6.2015-1226] Volltext nicht online.
Boztas, Soner and Liersch, Carsten M. (2016) Verifizierung des potenzialtheoretischen Strömungslösers CMARC anhand von Ergebnissen der Strömungslöser LIFTING_LINE und VSAERO. DLR-Interner Bericht. DLR-IB-AS-BS-2016-298, 57 S. Volltext nicht frei.
Brezillon, Joel and Carrier, Gerald and Laban, Martin (2010) Multi-Disciplinary Optimization Including Environmental Aspects Applied To Supersonic Aircraft. 27TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES, 19.-24. September 2010, Nizza, Frankreich.
Brezillon, Joel and Carrier, Gerald and Laban, Martin (2011) Multidisciplinary Optimization of Supersonic Aircraft Including Low-Boom Considerations. Journal of Mechanical Design, 133 (10), pp. 1-9. American Society of Mechanical Engineers (ASME). DOI: 10.1115/1.4004972 ISSN 1050-0472 Volltext nicht online.
Brezillon, Joel and Guntzer, Frederic (2010) Applications of modeFRONTIER on Aeronautical Problems: an overview of experiences at the German Aerospace Centre (DLR). International modeFRONTIER Users’ Meeting 2010, 27.-28. Mai 2010, Trieste, Italien. Volltext nicht online.
Brodersen, Olaf (1992) Untersuchung einer Matrix-Dissipation in einem Zelleneckpunkt-Finite-Volumen-Schema zur Lösung der Navier-Stokes-Gleichungen. Master's. DLR-Forschungsbericht. Volltext nicht online.
Brodersen, Olaf and Crippa, Simone and Eisfeld, Bernhard and Keye, Stefan and Geisbauer, Sven (2010) DLR Results from the Fourth AIAA CFD Drag Prediction Workshop. AIAA Applied Aerodynamics Conference, 28. Juni - 1. Juli 2010, Chicago, USA. Volltext nicht online.
Brodersen, Olaf and Monsen, Eric and Ronzheimer, Arno and Rudnik, Ralf and Rossow, Cord (1999) Computation of aerodynamic coefficients for the DLR-F6 configuration using MEGAFLOW. In: New Results in Numerical and Experimental Fluid Mechanics II, 72, pp. 85-92. Vieweg. 11th AG STAB/DGLR Symposium, 1998-11-10 - 1998-11-12, Berlin (DE). ISBN 3-528-03122-0 ISSN 0179-9614 Volltext nicht online.
Brodersen, Olaf and Rakowitz, Mark and Amant, Stephane and Larrieu, Pascal and Destarac, Daniel and Sutcliffe, Mark (2005) Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop. Journal of Aircraft, 42 (4), pp. 932-940. ISSN 0021-8669 Volltext nicht online.
Brodersen, Olaf and Ronzheimer, Arno and Keye, Stefan (2010) Calculation of Forces and Aerodynamics Effects of the Panasonic Radome installed on the A380. Other. DLR-Interner Bericht. DLR-IB 124-2010/914, 47 S. Volltext nicht online.
Brodersen, Olaf and Crippa, Simone (2014) RANS-based Aerodynamic Drag and Pitching Moment Predictions for the Common Research Model. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag. pp. 485-493. ISBN 978 3 319 03157 6. ISSN 1612-2909 Volltext nicht online.
Brodersen, Olaf and Crippa, Simone and Eisfeld, Bernhard and Keye, Stefan and Geisbauer, Sven (2009) DLR TAU Results for the AIAA 4th CFD Drag Prediction Workshopi. AIAA 4th CFD Drag Prediction Workshop, 20.-21. Juni 2009, San Antonio, Texas, USA.
Brodersen, Olaf and Laflin, Kelly (2016) DPW-VI Summary of Participant Data - CRM Cases 2-5: Trailing Edge Separation. 6th AIAA CFD Drag Prediction Workshop, 16.-17. Juni 2016, Washington D.C., USA. Volltext nicht online.
Brodersen, Olaf and Vassberg, John and Morrison, Joseph (2016) CRM Baseline Grids: Other Grids. 6th AIAA CFD Drag Prediction Workshop, 16.-17. Juni 2016, Washington D.C., USA. Volltext nicht online.
Campbell, Richard L. and Campbell, Matthew L. and Streit, Thomas (2011) Progress Toward Efficient Laminar Flow Analysis and Design. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, Hawaii, USA. Volltext nicht online.
Carrier, Gérald and Gebhardt, Lutz (2005) A Joint DLR-ONERA Contribution to CFD-based Investigations of Unconventional Empennages for Future Civil Transport Aircraft. In: 2005 CEAS/KATnet Conference on Key Aerodynamic Technologies. CEAS/KATnet Conference on Key Aerodynamic Technologies, 20 - 22 June 2005, Bremen, Germany, 2005-06-20 - 2005-06-22, Bremen (Germany).
Casper, Marcus and Scholz, Peter and Radespiel, Rolf and Wild, Jochen and Ciobaca, Vlad (2011) Separation Control on a High-Lift Airfoil using Vortex Generator Jets at High Reynolds numbers. 41st AIAA Fluid Dynamics Conference, 27.-30. Juni 2011, Honolulu, USA. Volltext nicht online.
Ciobaca, Vlad (2007) Assesment of blocking/mean flow effects in the Cepra19 w/t analyzed by means of CFD simulations. DLR-Interner Bericht. DLR-IB 124-2007/906, 38 S. Volltext nicht online.
Ciobaca, Vlad (2010) Parameter study for a slatless 2D high-lift airfoil with active separation control using a URANS approach. 17. DGLR-Fach Symposium der STAB, 09. - 10.11.2010, Berlin, Deutschland. Volltext nicht online.
Ciobaca, Vlad and Dandois, Julien and Bieler, Heribert (2012) A CFD BENCHMARK FOR FLOW SEPARATION CONTROL APPLICATION. Volltext nicht online.
Ciobaca, vlad and Kühn, Timo (2011) Active Separation Control on High-Lift Configurations using a URANS approach. ODAS 2011, 9-11 Februar 2011, Toulouse, Frankreich. Volltext nicht online.
Ciobaca, Vlad (2008) Simulation of active flow control on the flap of a 2D high-lift configuration. New Results in Numerical and Experimental Fluid Mechanics VII, 112 (pp. 20). Springer Verlag. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht frei.
Ciobaca, Vlad (2014) Validation of numerical simulations for separation control on high-lift configurations. Dissertation, DLR, Institut für Aerodynamik und Strömungstechnik. Volltext nicht online.
Ciobaca, Vlad and Dandois, Julien (2015) Numerical Optimization of a Zero-Net-Mass-Flux Actuation for a High Lift Airfoil. European Drag Reduction and Flow Control Meeting – EDRFCM 2015, 23.–26. März 2015, Cambridge, UK. Volltext nicht frei.
Ciobaca, Vlad and Dandois, Julien and Bieler, Heribert (2014) A CFD Benchmark for Flow Separation Control Application. International Journal of Flow Control, 6 (3), pp. 67-81. Sage Publications. ISBN ISSN 1756-8250 ISSN 1756-8250 Volltext nicht frei.
Ciobaca, Vlad and Kühn, Timo and Rudnik, Ralf and Bauer, Matthias and Gölling, Burkhard and Breitenstein, Wiebke (2013) Active Flow-Separation Control on a High-Lift Wing-Body Configuration. Journal of Aircraft (2013, ), pp. 56-72. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C031659 ISSN 0021-8669 Volltext nicht frei.
Ciobaca, Vlad and Rudnik, Ralf and Huacke, Frank and Nitsche, Wolfgang (2013) Active Flow Control on a High-Lift Airfoil: URANS Simulations and Comparison with Time-Accurate Measurements. 31st AIAA Applied Aerodynamics Conference, June 24-27, 2013, San Diego, CA. Volltext nicht frei.
Ciobaca, Vlad and Wild, Jochen (2014) Active Flow Control for an Outer Wing Model of a Take-off Transport Aircraft Configuration - A Numerical Study. In: AIAA 32nd Applied Aerodynamics Conference. AIAA Applied Aerodynamics Conferece, Atlanta, 16.-20- Juni. 2014, USA. Volltext nicht frei.
Ciobaca, Vlad and Wild, Jochen and Bauer, Matthias and Grund, Thomas and Hühne, Philipp and Scholz, Peter and Stefes, Bruno (2015) Wind Tunnel Experiments with Active Flow Control for an Outer Wing Model. 33rd AIAA Applied Aerodynamics Conference, 22.-26. Jun. 2015, Dallas, TX, USA. DOI: 10.2514/6.2015-2728 Volltext nicht frei.
Ciobaca, vlad and Kühn, Timo and Rudnik, Ralf and Bauer, Matthias and Gölling, Burkhard (2011) Active Flow Separation Control on a High-Lift Wing-Body Configuration. Part 2: The Pulsed Blowing Application. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011,, Honolulu, Hawaii.
Ciobaca, vlad and Wild, Jochen (2013) An Overview of Recent DLR Contributions on Active Flow-Separation Control Studies for High-Lift Configurations. Aerospace Lab, Issue . ISSN 2107-6596 Volltext nicht frei.
Cummings, R. and Schütte, A. (2010) An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimations: Overview of NATO RTO AVT-161. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 01. Juli 2010, Chicago, USA. Volltext nicht online.
Cummings, Russel M. and Schütte, Andreas and Hübner, Andreas-Rene (2013) Overview of Stability and Control Estimation Methods from NATO Task Group AVT-201. AIAA. 51st AIAA Aerospace Sciences Meeting, 07. - 10. Jan. 2013, Dallas, Texas, USA. Volltext nicht online.
Cummings, Russel M. and Schütte, Andreas (2013) Detached-Eddy Simulation of the vortical flow field about the VFE-2 delta wing. Aerospace Science and Technology, 24 (1), pp. 66-76. Elsevier. DOI: 10.1016/j.ast.2012.02.007 ISSN 1270-9638 Volltext nicht online.
Cummings, Russel M. and Schütte, Andreas (2012) Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation. Journal of Aircraft, 49 (6), pp. 1542-1557. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C031430 ISSN 0021-8669 Volltext nicht online.
Cummings, Russel M. and Schütte, Andreas (2014) The NATO STO Task Group AVT-201 on ‘Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles’. In: 32nd AIAA Applied Aerodynamics Conference. 32nd AIAA Applied Aerodynamics Conference, 16.-20. Juni 2014, Atlanta, GA, USA. Volltext nicht online.
Cummings, Russel M. and Schütte, Andreas (2016) THE NATO STO TASK GROUP AVT-201. NATO STO - Science and Technology Organisation. [Other] Volltext nicht online.
Cummings, Russel, M and Schütte, Andreas (2008) Detached-Eddy Simulation of the Vortical Flowfield about the VFE-2 DeltaWing. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, Nevada, USA. Volltext nicht frei.
Egami, Yasuhiro and Fey, Uwe and Klein, Christian and Sitzmann, Martin and Wild, Jochen (2006) Transition Detection on High-Lift devices in DNW-KKK by means of Temperature-Sensitive Paint. Optimage Ltd. Edinburgh, UK. 12th International Symposium on Flow Visualization, 2006-09-10 - 2006-09-14, Göttingen, Germany. Volltext nicht online.
Egami, Yasuhiro and Fey, Uwe and Klein, Christian and Sitzmann, Martin and Wild, Jochen (2006) Transition Detection on High-Lift Devices in the DNW-KKK by means of Temperature-Sensitive Paint. Other. Volltext nicht online.
Egami, Yasuhiro and Klein, Christian and Henne, Ulrich and de Groot, Klaus and Meyer, Jörg B. and Krückeberg, Claus-Peter and Boden, Fritz (2013) In-Flight Application of Pressure Sensitive Paint. In: Research Topics in Aerospace Advanced In-Flight Measurement Techniques. Springer Verlag, Heidelberg New York Dordrecht London. pp. 237-267. ISBN 978-3-642-34737-5 . ISSN 2194-8240 Volltext nicht online.
Enk, Stephan (2007) Ein Verfahren höherer Ordnung in FLOWer für LES. DLR-Interner Bericht. DLR-IB 124-2007/8, 51 S. Volltext nicht online.
Enk, Stephan (2008) A Fourth Order Finite Difference Method for Large Eddy Simulation at a Flate Plate. STAB Symposium 2008, 2008-11-3 -2008-11-4, Aachen. Volltext nicht online.
Enk, Stephan (2010) DES an einer Tranportflugzeugkonfiguration mit offener Heckrampe. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.
Enk, Stephan (2015) Zellzentriertes Padeverfahren für DNS und LES. Dissertation. DLR-Forschungsbericht. DLR-FB 2015-24, 121 S. Volltext nicht online.
Franke, Dirk M. (2010) Aerodynamic Optimization of a High-Lift System with Kinematic Constraints. 17. DGLR-Fach Symposium der STAB, 09. - 10.11.2010, Berlin, Deutschland.
Franke, Dirk M. (2012) Multidisciplinary Optimization of a Generic 2D High-Lift Configuration Regarding Kinematics, Aerodynamics and Flight Mechanics. 30th AIAA Applied Aerodynamics Conference, 25.06.-28.06.2012, New Orleans, USA. Volltext nicht frei.
Franke, Dirk M. (2015) Investigation on continuously deflectable High-Lift Devices for a 3D High-Lift Configuration. 33rd AIAA Applied Aerodynamics Conference, Aviation Forum 2015, 22. - 26. Jun. 2015, Dallas, USA. DOI: 10.2514/6.2015-2258 Volltext nicht frei.
Franke, Dirk M. and Wild, Jochen (2014) Aerodynamic Design of a Folded Krüger Device for a HLFC Wing. 19. DGLR-Fachsymposium der STAB, 4.-5.11. 2014, München.
Franke, Dirk M. and Wild, Jochen (2016) Aerodynamic Design of a Folded Krüger Device for a HLFC Wing. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer Verlag. pp. 17-27. ISBN 978-3-319-27278-8. ISSN 1612-2909 Volltext nicht frei.
Fricke, Sebastian and Ciobaca, Vlad and Kröhnert, Anna and Wild, Jochen and Blesbois, Olivier (2015) Active Flow Control Applied at the Engine-Wing Junction. 5th CEAS Air and Space Coneference, 7.-12. Sept. 2015, Delft, Niederlande. Volltext nicht frei.
Fricke, Sebastian and Ciobaca, Vlad and Wild, Jochen and Normab, David (2015) Numerical Studies of Active Flow Control applied at the Engine-Wing Junction. In: Advances in Simulation of Wing and Nacelle Stall Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 131. Springer Verlag. pp. 397-411. ISBN ISBN: 978-3-319-21126-8 (Print) 978-3-319-21127-5 (Online). ISSN 1612-2909 Volltext nicht frei.
Fricke, Sebastian and Ciobaca, Vlad and Wild, Jochen and Norman, David (2014) Numerical Studies of Active Flow Control applied at the Engine-Wing Junction. Joint Symposium of DFG FOR 1066 and DLR C²A²S²E: "Simulation of Wing and Nacelle Stall", 01.-02. Dez. 2014, Braunschweig, Deutschland. Volltext nicht online.
Gauger, Nicolas and Ilic, Caslav and Schmidt, Stephan and Schulz, Volker (2012) Non-parametric aerodynamic shape optimization. In: Mathematics and Statistics, 160 (2). Springer. pp. 289-300.
Gazaix, Anne and Gendre, Pascal and Chaput, Eric and Blondeau, Christophe and Carrier, Gérald and Schmollgruber, Peter and Brezillon, Joël and Kier, Thiemo (2011) Investigation of Multi-Disciplinary Optimisation for Aircraft Preliminary Design. SAE 2011 AeroTech Congress & Exhibition, 18-21 Oct. 2011, Toulouse, Frankreich. Volltext nicht online.
Gebhardt, Lutz and Weber, Carsten and Enk, Stephan and Joel, Brezilion (2008) Numerical Optimization on the Vertical Tailplane of Transport Aircraft. STAB Symposium 2008, 2008-11-3 -2008-11-4, Aachen. Volltext nicht online.
Gebhardt, Anna and Kirz, Jochen (2016) Numerical Investigation of Slot Variations on the Efficiency of Tangential Blowing at a Vertical Tailplane with Infinite Span. DLRK 2016, 13.-15. Sept. 2016, Braunschweig, Deutschland. Volltext nicht online.
Gebhardt, Anna and Kirz, Jochen (2016) Numerical Investigation of Slot and Configuration Impact on the Efficiency of Tangential Blowing at a Vertical Tailplane with Infinite Span. 20. DGLR-Fach-Symposium der STAB, 08.-09. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online.
Gebhardt, Anna and Kirz, Jochen (2016) Numerical Investigation of Slot Variations on the Efficiency of Tangential Blowing at a Vertical Tailplane with Infinite Span. In: urn:nbn:de:101:1-201611255167. DLRK 2016, 13.-15. Sept. 2016, Braunschweig, Deutschland. Volltext nicht online.
Gebhardt, Lutz and Kröhnert, Anna (2014) Heck- und Leitwerksaerodynamik. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag München. pp. 192-212. ISBN 978-3-446-42341-1. Volltext nicht online.
Geisbauer, Sven (2010) Unsteady CFD Calculations of Pitching Motions for the DLR-F6 Configuration. DLR-Interner Bericht. DLR-IB 124-2010/1, 56 S. Volltext nicht frei.
Geisbauer, Sven (2011) Unsteady CFD Calculations of Pitching and Heave Motions for the DLR-F6 Configuration. DLR-Interner Bericht. DLR-IB 124-2011/1, 71 S. Volltext nicht frei.
Geisbauer, Sven (2012) Untersuchung des Einflusses generischer Vorderkantenbeschädigungen auf die aerodynamische Leistungsfähigkeit von Flugzeugprofilen. DLR-Interner Bericht. DLR-IB 124-2012/903, 50 S. Volltext nicht online.
Geisbauer, Sven (2013) Dokumentation einer Prozesskette zur Simulation von Lastabsetzvorgängen. DLR-Interner Bericht. DLR-IB 124-2013/915, 31 S. Volltext nicht frei.
Geisbauer, Sven and Bier, Niko and Kirz, Jochen and Roosenboom, Eric (2013) Title confidential. DLR-Interner Bericht. DLR-IB 124-2013/910, 145 S. Volltext nicht online.
Geyr, Frfr. von, Judith and Knoblauch zu Hatzbach, von, Fedime and Streit, Thomas and Wichmann, Georg (2014) Wing Design Based on a Tapered Wing Natural Laminar Flow Airfoil Catalogue. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag. pp. 183-191. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.
Haar, Danil and Brezillon, Joel (2011) Engine Integration Based on Multi-Disciplinary Optimisation Technique. 11th ONERA-DLR Aerospace Symposium (ODAS) 2011, 9-11 February, 2011, Toulouse.
Haar, Danil and Brezillon, Joel (2011) Engine integration based on multidisciplinary optimisation technique. CEAS Aeronautical Journal. Springer. DOI: 10.1007/s13272-011-0013-9 Volltext nicht online.
Haar, Danil (2009) Engine integration based on high-fidelity optimisation technique. KATnet II Conference on Key Aerodynamic Technologies, 12.-14. Mai 2009, Bremen, Germany.
Hatanaka, Keita and Brezillon, Joel and Ronzheimer, Arno (2012) A FULLY AUTOMATED CAD-BASED FRAMEWORK FOR SHAPE OPTIMIZATION. 28TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES, September 23rd to 28th, 2012, Brisbane, Australia. Volltext nicht online.
Heidebrecht, Alexander (2014) Untersuchungen zur Modellierung und Simulation der transsonischen Messstrecke des ETW. Dissertation. DLR-Forschungsbericht. DLR-FB 2014-13, 117 S. Volltext nicht online.
Hepperle, Martin (2012) Electric Flight - Potential and Limitations. Energy Efficient Technologies and Concepts of Operation, 22-24 October 2012, Lisbon, Portugal.
Hepperle, Martin (2016) Case Study: Electric Powered Do 228. DLR-Forschungsbericht. DLR-IB-AS-BS-2016-144, 35 S. Volltext nicht frei.
Hepperle, Martin (2015) Propeller für elektrisch angetriebene Flugzeuge. Symposium Elektrisches Fliegen, 26.-27. Februar 2015, Stuttgart.
Hepperle, Martin (2016) Aspects of Distributed Propulsion - A View on Regional Aircraft. Symposium Elektrisches Fliegen, 18.-19. Februar 2016, Stuttgart.
Himisch, Jan and Melber-Wilkending, Stefan and Horstmann, K.H. (2006) Anwendung von modernen CFD-Verfahren fuer den Segelflug - Numerische Untersuchungen der Stroemungseffekte im Kreisflug. 30th Segelflugsymposium, Darmstadt, 23.-24. Nov. 2006, Darmstadt, Deutschland. Volltext nicht online.
Hoheisel, Heinz and Frhr. von Geyr, Heiko (2012) The influence of engine thrust behaviour on the aerodynamics of engine airframe integration. CEAS Aeronautical Journal, 3 (1), pp. 79-92. Springer. DOI: 10.1007/s13272-012-0044-x Volltext nicht online.
Homeyer, Tim and Kampers, Gerrit and Manso Jaume, Ana and Wild, Jochen and Peinke, Joachim and Gülker, Gerd and Hölling, Michael (2014) Wind tunnel measurements on the influence of turbulence on polars and flow separation of an airfoil. 10th Euromech Fluid Mechanics Conference, 10.-14. Sep. 2014, Kopenhagen, Dänemark. Volltext nicht online.
Horstmann, Karl Heinz (2014) Flügelentwurf. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag München. pp. 173-184. ISBN 978-3-446-42341-1. Volltext nicht online.
Huber, Kerstin Claudie (2010) Numerical Investigation of the Aerodynamic Properties of a Flying Wing Configuration. DLR-Interner Bericht. DLR-IB 124-2010/4, 105 S. Volltext nicht online.
Hübner, Andreas-Rene and Vicroy, Dan D. and Schütte, Andreas and Huber, Kerstin (2011) Experimental and Numerical Investigation of Dynamic Derivatives of an UCAV Configuration. In: NATO RTO Meeting Proceedings (RTO-AVT-MP-189), 23-1-23-20. NATO RTO. NATO RTO AVT Specialists' Meeting on "Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles", 12.-14. Oct. 2011, Portsdown, UK. Volltext nicht online.
Hühne, Claus-Philipp and Scholz, Peter and Radespiel, Rolf and Wild, Jochen and Ciobaca, Vlad (2012) Active Control of Leading Edge Flow Separation for a Swept High-Lift Airfoil. Deutscher Luft- und Raumfahrtkongress 2012, 10.-12. Sept. 2012, Berlin. Volltext nicht online.
Hübner, Andreas-René and Vicroy, Dan and Schütte, Andreas and Huber, Kerstin Claudie (2011) Experimental and Numerical Investigation of Dynamic Derivatives of an UCAV Configuration. RTO / AVT-189/RSM-028 Specialists’ Meeting, 12.-14. Okt. 2011 , Schottland. Volltext nicht online.
Hübner, A.-R. and Vicroy, Dan D. and Schütte, Andreas and Huber, Kerstin Claudie (2011) Experimental and Numerical Investigation of Dynamic Derivatives of an UCAV Configuration. In: NATO RTO-AVT Specialists' Meeting Proceddings RTO-AVT-MP-189 on "Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles" (23). NATO RTO - Research and Technology Organisation. NTO RTO AVT Specialists' Meeting on "Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles", Portsdown, UK. DOI: 10.14339/RTO-MP-AVT-189 Volltext nicht online.
Iannelli, Pierluigi and Wild, Jochen and Minervino, Mauro and Strüber, Henning and Moens, Frederic and Vervliet, Antoon (2013) Design of a High-Lift System for a Laminar Wing. In: Proceedings CD-Rom. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 1.-4. Juli 2013, München, Deutschland.
Ilic, Caslav (2013) Adjoint gradient-based approach for aerodynamic optimization of transport aircraft. European Conference on Computational Optimization (EUCCO), July 17-19, 2013, Chemnitz, Germany.
Ilic, Caslav and Brezillon, Joël (2011) Optimization of an airfoil polar in transonic RANS flow using an adjoint gradient-based approach. 15. STAB-Workshop, 9-10 Nov 2011, Göttingen, Germany.
Jirasek, Adam and Cummings, Russel M. and Schütte, Andreas and Huber, Kerstin Claudie (2014) The NATO STO AVT-201 Task Group on Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles: Summary, Conclusions and Lessons Learned. In: 32nd AIAA Applied Aerodynamics Conference (2394). American Institute of Aeronautics and Astronautics. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA. Volltext nicht online.
Keller, Dennis (2012) Numerische Untersuchung der statischen Längstabilität eines Transportflugzeugs mit Zirkulationskontrolle. 18. DGLR-Fach-Symposium der STAB, 6.-7. Nov. 2012, Stuttgart. Volltext nicht online.
Keller, Dennis (2013) Numerical Investigation of Engine Effects on the Stability and Controllability of a Transport Aircraft with Circulation Control. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego, USA. Volltext nicht online.
Keller, Dennis (2014) Numerical Approach Aspects for the Investigation of the Longitudinal Static Stability of a Transport Aircraft with Circulation Control. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer. pp. 13-22. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.
Keller, Dennis (2016) Numerical Simulation of a Fully Integrated Engine Ground Test. 54th AIAA Aerospace Sciences Meeting, 4-8 Jan 2016, San Diego, Ca, USA. Volltext nicht online.
Keller, Dennis and Rudnik, Ralf (2013) Aerodynamic Aspects of the Longitudinal Motion of a High-Lift Aircraft Conﬁguration with Circulation Control. Project Report. Shaker Verlag.
Keller, Dennis and Rudnik, Ralf (2015) Numerical Investigation of Engine Effects on a Transport Aircraft with Circulation Control. Journal of Aircraft, 52 (2), pp. 421-438. American Institute of Aeronautics and Astronautics (AIAA). ISSN 0021-8669 Volltext nicht online.
Keller, Dennis and Rudnik, Ralf (2015) Numerical Investigations of Aerodynamic Properties of a Propeller Blown Circulation Control System on a High Wing Aircraft. In: 3AF - Aerodynamics 2015. Aerodynamics 2015, 30. März - 1. April 2015, Toulouse, Frankreich. Volltext nicht online.
Keller, Dennis and Rudnik, Ralf (2015) Integration Aspects of Lift Augmentation Systems on the Aerodynamics of a High-Lift Configuration. Project Report. Volltext nicht online.
Keller, Dennis and Rudnik, Ralf (2015) Numerical Investigation of the Dynamic Behavior of a High Lift Configuration with Circulation Control. In: AIAA 33rd Applied Aerodynamics Conference. AIAA - Aviation 2015, Dallas, USA. Volltext nicht online.
Keller, Dennis and Rudnik, Ralf and Hasan, Yasim (2016) NACELLE STRAKE DESIGN FOR A SHORT TAKE-OFF AND LANDING CONFIGURATION WITH TURBOPROPS. European Congress on Computational Methods in Applied Sciences and Engineering 2016, 5-10 Juni 2016, Hersonissos, Greece. Volltext nicht online.
Keller, Dennis and Wild, Jochen (2014) High-Lift Concepts Compatible with Laminar Flow Wings. DLR-Interner Bericht. DLR-IB 124-2014/915, 17 S. Volltext nicht online.
Keye, Stefan (1993) Experimental Wall Interference Assessment for a DLR R4C Airfoil in the Transonic Variable Slotted Wall Test Section of the VKI-S1 Wind Tunnel. Other. Other. VKI-PR 1993-04. Volltext nicht online.
Keye, Stefan (2011) Fluid-Structure Coupled Analysis of a Transport Aircraft and Flight Test Validation. Journal of Aircraft, Vol. 48 (2), pp. 381-390. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C000235 Volltext nicht online.
Keye, Stefan (2012) Simulation eines vollständig elastischen Transportflugzeugs mit Hilfe der Strömungs-Struktur-Kopplung. 18. DGLR-Fach-Symposium der STAB, 6.-7. November 2012, Stuttgart, D. Volltext nicht online.
Keye, Stefan (2011) Analyse der vollständigen Hochauftriebskonfiguration des Transportflugzeugs Airbus A350-900 XWB mit Hilfe der Fluid-Struktur-Kopplung. DLR-Interner Bericht. DLR-IB 124-2011/910, 24 S. (Unpublished) Volltext nicht online.
Keye, Stefan and Rudnik, Ralf (2009) Aero-Elastic Simulation of DLR’s F6 Transport Aircraft Configuration and Comparison to Experimental Data. In: 48th AIAA Aerospace Sciences Meeting. 48th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, FL (USA). Volltext nicht online.
Keye, Stefan and Sitzmann, Martin and Brodersen, Olaf and Heinrich, Ralf (2008) Fluid-Structure Coupled Loads Analysis of DLR’s F6 Wing-Body Configuration. In: 46th AIAA Aerospace Sciences Meeting, 2008. 46th AIAA Aerospace Sciences Meeting, 2008, 7.1.2008-10.1.2008, Reno, NV (USA). Volltext nicht online.
Keye, Stefan (2009) Fluid-Structure-Coupled Analysis of a Transport Aircraft and Comparison to Flight Data. 39th AIAA Fluid Dynamics Conference, 22 - 25 June 2009, San Antonio, TX (USA). Volltext nicht online.
Keye, Stefan (2014) An Assessment of the Influence of Fuselage Deformations on the Numerical Prediction of High-Lift Performance. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. pp. 385-393. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.
Keye, Stefan and Brodersen, Olaf and Rivers, Melissa, B. (2014) Investigation of Aeroelastic Effects on the NASA Common Research Model. Journal of Aircraft, 51 (4), pp. 1323-1330. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C032598 ISSN 0021-8669 Volltext nicht online.
Keye, Stefan and Gammon, Mark (2016) Development of Deformed CAD Geometries of NASA's Common Research Model for the 6th AIAA CFD Drag Prediction Workshop. 34th AIAA Applied Aerodynamics Conference, 13.-17.6.2016, Washington, D.C., USA. Volltext nicht frei.
Keye, Stefan and Mavriplis, dimitri (2016) DPW-6 Summary of Participant Data Test Case 5 CRM WB Coupled Aero-Structural Simulation. 6th AIAA CFD Drag Prediction Workshop, 16.-17.6.2016, Washington, DC, USA. Volltext nicht frei.
Keye, Stefan and Rudnik, Ralf (2015) Validation and Assessment of Turbulence Model Impact for Fluid-Structure Coupled Computations of the NASA CRM. In: CEAS Aeronautical Journal. 5th CEAS Air & Space Comference, 7.-11.9.2015, Delft, NL. Volltext nicht frei.
Kilian, Thomas (2016) Experimental Investigation of Generic Ice Block Trajectories under Freestream Conditions. DLRK 2016, 13.-15. Sep. 2016, Braunschweig, Deutschland. Volltext nicht online.
Kirz, Jochen (2016) Numerische Strömungssimulation von Schlitzvariationen bei tangentialem Ausblasen über dem Ruder an einem gepfeilten Seitenleitwerk unendlicher Streckung. Master's. Volltext nicht online.
Kompenhans, Jürgen and Pallek, Dieter and von Geyr, Heiko and Schröder, Andreas (2009) Experimental and Numerical Study on the Flow behind a TPS. Seminar China Aerodynamics Research and Development Center (CARDC), 27.03.2009, Mianyang, China. Volltext nicht online.
Kruse, Martin and Küpper, Albert and Petzold, Rouven and Munoz, Federico (2016) Bestimmung des kritischen N-Faktors für Querströmungsinstabilität für den Niedergeschwindigkeits-Windkanal Braunschweig (DNW-NWB). 20. DGLR Fach-Symposium der STAB, 08.-09.11.2016, TU Braunschweig. Volltext nicht online.
Kröhnert, Anna and Gebhardt, Lutz (2013) Investigation of the impact of simplifying the aircraft geometry on the characteristics of the vertical tailplane. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 121. Springer Verlag. pp. 1-8. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.
Kröhnert, Anna and Gebhardt, Lutz (2012) The Influence of geometric Simplifications of an Aircraft with Respect to the Optimization of the Aerodynamic Characteristics of the Vertical Tailplane. Deutscher Luft- und Raumfahrtkongress 2012, 10.-12. Sept. 2012, Berlin, Deutschland. Volltext nicht online.
Kröhnert, Anna (2014) Title confidential. DLR-Interner Bericht. DLR-IB 124-2014/904, 62 S. Volltext nicht online.
Kröhnert, Anna (2014) Title confidential. DLR-Interner Bericht. DLR-IB 124-2014/903, 112 S. Volltext nicht online.
Kröhnert, Anna (2012) Titel confidential. DLR-Interner Bericht. DLR-IB 124-2012/915, 32 S. Volltext nicht online.
Kröhnert, Anna (2014) Numerical Investigation of Tangential Blowing at the Rudder of a Vertical Tailplane Airfoil. In: 32nd AIAA Applied Aerodynamics Conference. 32nd AIAA Applied Aerodynamics Conference, AIAA Aviation and Aeronautics Forum and Exposition 2014, 16.-20. Juni 2014, Atlanta, Georgia, USA. Volltext nicht online.
Kröhnert, Anna (2014) Numerical Investigation of Unsteady Tangential Blowing at the Rudder of a Vertical Tailplane Airfoil. 19. DGLR-Fach-Symposium der STAB, 4.-5. November 2014, München. Volltext nicht online.
Kröhnert, Anna (2015) Title confidential. DLR-Interner Bericht. DLR-IB 124-2015/906, 74 S. Volltext nicht online.
Kröhnert, Anna (2016) Numerical Investigation of Unsteady Tangential Blowing at the Rudder of a Vertical Tailplane Airfoil. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer Verlag. pp. 39-49. ISBN 978-3-319-27278-8. ISSN 1612-2909 Volltext nicht online.
Kröhnert, Anna and Gebhardt, Lutz (2010) Untersuchung des Einflusses der Vereinfachung der Flugzeuggeometrie auf die Charakteristiken des Seitenleitwerks. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.
Krüger, Wolf and Cumnuantip, Sunpeth and Liersch, Carsten M. (2011) Multidisciplinary Conceptual Design of a UCAV Configuration. In: Proceedings AVT-MP173. RTO/AVT Panel Workshop "Virtual Prototyping of Affordable Military Vehicles Using Advanced MDO", 16.-18. Mai 2011, Sofia, Bulgarien. Volltext nicht online.
Kwak, Dongyoun and Gaffuri, Michele and Ohira, Keisuke and Brezillon, Joël (2012) Numerical Study of the Reynolds Number Effect on Low Aspect Ratio Wing at Low Speed. 28th Congress of the International Council of the Aeronautical Sciences , 23-28 Sep 2012, Brisbane, Australia. ISBN 978-0-9565333-1-9 Volltext nicht online.
Kwak, Dongyoun and Ohira, Keisuke and Rudnik, Ralf (2014) Reynolds number effect on vortex dominant flow on the SST configurations. APISAT2014, 24.-26. Sept. 2014, Shanghai, China. Volltext nicht online.
Kühn, Timo and Ciobaca, Vlad and Rudnik, Ralf and Gölling, Burkhard and Breitenstein, Wiebke (2010) Pilot Study of a High Lift Wing Configuration for Performance Optimization. Joint Symposium of DFG FOR 1066 and DLR-Airbus CASE, Braunschweig, Germany. (Unpublished) Volltext nicht online.
Kühn, Timo and Ciobaca, Vlad and Rudnik, Ralf and Gölling, Burkhard and Breitenstein, Wiebke (2011) Active Flow Separation Control on a High-Lift Wing-Body Configuration - Part 1: Baseline Flow and Constant Blowing. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, HI, USA.
Kühn, Timo and Lenfers, Carsten (2012) A Numerical Assessment of Side Plate Effects for a Low Aspect Ratio Wind Tunnel Model with a Smart Droop Nose Device. 30th AIAA Applied Aerodynamics Conference, 25-28 June 2012, New Orleans, LA, USA. Volltext nicht online.
Kühn, Timo and Wild, Jochen (2010) Aerodynamic Optimization of a Two-Dimensional Two-Element High Lift Airfoil with a Smart Droop Nose Device. 1st EASN Association Workshop on Aerostructures, Paris, France. (Unpublished) Volltext nicht online.
Kühn, Timo (2013) Aerodynamische Vermessung lärmarmer Hochauftriebssysteme im Rahmen des DLR-Projekts SLED. Other. DLR-Interner Bericht. DLR-IB 124-2013/908, 108 S. Volltext nicht online.
Landa, Tim and Radespiel, Rolf and Wild, Jochen (2015) Numerical Simulations of Streamwise Vortices on a High-Lift Wing. Deutscher Luft- und Raumfahrtkongress (DLRK) 2015, 22.-24. Sep. 2015, Rostock, Germany. Volltext nicht online.
Landa, Tim and Radespiel, Rolf and Wild, Jochen (2016) Numerical Simulations of Streamwise Vortices on a Generic High-Lift Configuration. 54th AIAA Aerospace Sciences Meeting, 4.-8. Januar 2016, San Diego, CA, USA. DOI: 10.2514/6.2016-0304 Volltext nicht online.
Landa, Tim and Wild, Jochen and Radespiel, Rolf (2014) Simulation of Longitudinal Vortices on a High-Lift Wing. Symposium "Simulation of Wing and Nacelle Stall", 1.-2. Dez. 2014, Braunschweig. Volltext nicht online.
Landa, Tim and Wild, Jochen and Radespiel, Rolf (2015) Simulation of Longitudinal Vortices on a High-Lift Wing. In: Advances in Simulation of Wing and Nacelle Stall Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 131. Springer. pp. 351-366. ISBN 978-3-319-21127-5. ISSN 1612-2909 Volltext nicht online.
Lange, Fabian (2015) Experimentelle Untersuchungen an einem gepfeilten Hochauftriebsflügel mit Strömungskontrolle. Other. DLR-Interner Bericht. DLR-IB 124-2015/902, 100 S. Volltext nicht online.
Lenfers, Carsten (2012) Propeller Design for a future QESTOL Aircraft in the BNF Project. AIAA Applied Aero 2012, 25.-28.06.2012, USA, New Orleans. Volltext nicht frei.
Lenfers, Carsten (2013) Computational Investigation of the DLR Reference Noise Source in the AWB - Contribution to Garteur AG 50. DLR-Interner Bericht. DLR-IB 124-2013/1, 40 S. Volltext nicht frei.
Lenfers, Carsten and Beck, Nils and Bauer, Marc (2016) Propeller and Active High Lift Wing Interaction in Experiment and Simulation. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer Verlag. pp. 51-61. ISBN 978-3-319-27278-8. ISSN 1612-2909 Volltext nicht online.
Levy, David and Laflin, Kelly and Tinoco, Edward and Vassberg, John and Mani, Mori and Rider, Ben and Rumsey, Christopher and Wahls, Richard and Morrison, Joseph and Brodersen, Olaf and Crippa, Simone and Mavriplis, Dimitri and Murayama, Mitsuhiro (2014) Summary of Data from the Fifth Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 51 (4), pp. 1194-1213. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C032389 ISSN 0021-8669 Volltext nicht online.
Liersch, Carsten M. and Hepperle, Martin (2011) A distributed toolbox for multidisciplinary preliminary aircraft design. 60. Deutscher Luft- und Raumfahrtkongress 2011, 27.-29. Sept. 2011, Bremen, Deutschland. Volltext nicht online.
Liersch, Carsten M. and Hepperle, Martin (2011) A distributed toolbox for multidisciplinary preliminary aircraft design. CEAS Aeronautical Journal, Volume 2 (Number 1-4), pp. 57-68. Springer. DOI: 10.1007/s13272-011-0024-6 ISSN 1669-5582 Volltext nicht online.
Liersch, Carsten M. and Huber, Kerstin Claudie (2014) Conceptual Design and Aerodynamic Analyses of a Generic UCAV Configuration. In: 32nd AIAA Applied Aerodynamics Conference (2001). 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA.
Löser, T. and Vicroy, D. and Schütte, A. (2010) SACCON Static Wind Tunnel Tests at DNW-NWB and 14'x22' NASA LaRC. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 01. Juli 2010, Chicago, USA. Volltext nicht online.
Lüdeke, Heinrich (2013) Validierung eines impliziten finite-Differenzen Verfahrens für Direkte Numerische Simulationen. 16. Stab-Workshop, 12.-13. Nov. 2013, Göttingen, Deutschland. Volltext nicht online.
Lüdeke, Heinrich (2014) Influences of a Rippled Surface on Growth Rates of Tollmien-Schlichting Waves. In: IUTAM Symposium on Laminar-Turbulent Transition. IUTAM-ABCM Symposium on Laminar-Turbulent Transition, 8.-12. Sept. 2014, Rio de Janeiro, Brazil. Volltext nicht online.
Lüdeke, Heinrich (2014) Interior Flow Simulation of Suction Chambers for HLFC Profiles. In: DLRK Beitrag. 63. Deutscher Luft- und Raumfahrtkongress 2014, 16.-18. September 2014, Augsburg, Germany. Volltext nicht online.
Lüdeke, Heinrich (2016) Towards a Validated DNS-Solver by Using the DLR FLOWer-Code with a Fourth Order Finite-Difference Method. DLR-Interner Bericht. DLR-IB-AS-BS-2016-44, 36 S. Volltext nicht online.
Lüdeke, Heinrich and Backhaus, Kai (2016) Direct Numerical Simulation of TS-Waves Behind a Generic Step of a laminar Profile in the DNW-NWB wind tunnel. Greener Aviation 2016, 11.-13. Okt. 2016, Brüssel, Belgien.
Lüdeke, Heinrich and Backhaus, Kai (2016) Direct TS-Wave Simulation Behind the Generic Step of a Laminar Wing-Profile in the DNW-NWB Wind-Tunnel. STAB 2016, 8.-9. Nov. 2016, Braunschweig, deutschland. Volltext nicht online.
Manso Jaume, Ana and Wild, Jochen (2014) Aerodynamic Design and Optimization of a High Lift Device for a Wind Turbine Airfoil. Jahrestagung der STAB, 04.-05. Nov. 2014, München, Deutschland. Volltext nicht frei.
Manso Jaume, Ana and Wild, Jochen (2014) Entwurf eines Vorflügels in integrierter sowie aufgesetzter Bauweise an dem DU 91-W2-250 Profil des Smart Blades Referenzblattes. DLR-Interner Bericht. DLR-IB 124-2014/7, 16 S.
Manso Jaume, Ana and Wild, Jochen (2016) Aerodynamic Design and Optimization of a High-Lift Device for a Wind Turbine Airfoil. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer. pp. 859-869. ISBN 978-3-319-27278-8. ISSN 1612-2909 Volltext nicht online.
Manso Jaume, Ana and Wild, Jochen and Homeyer, Tim and Hölling, Michael and Peinke, Joachim (2015) Design and Wind Tunnel Testing of a Leading Edge Slat for a Wind Turbine Airfoil. Deutscher Windenergie Kongress (DEWEK) 2015, 19.-20. Mai 2015, Bremen, Germany. Volltext nicht online.
Marquez, Carlos (2009) Steady Simulation of an Isolated Helicopter Rotor in Hover Configuration with the DLR TAU-Code. [Other] (Unpublished) Volltext nicht frei.
Marquez Gutierrez, Carlos Omar (2013) Title confidential. DLR-Interner Bericht. DLR-IB 124-2013/909, 95 S. Volltext nicht online.
Marquez Gutierrez, Carlos Omar and Steiner, Sören (2013) Analysis of a CROR Propulsion System at High Angle of Attack and at Low Speed Flight Conditions. 13th ONERA-DLR Aerospace Symposium, 27.-29. Mai 2013, Palaiseau, France. Volltext nicht frei.
Marquez Gutierrez, Carlos Omar and Steiner, Sören (2014) Aerodynamic Installation Effects of CROR Engines at Take-off Configurations. AIAA SciTech 2014 Conference, 13-17 Januar 2014, National Harbor, Maryland. Volltext nicht frei.
Marquez Gutierrez, Carlos Omar and Steiner, Sören and Fuss, Uwe (2013) Installation Aerodynamics of Open Rotor Engines: An Overview of The LuFo IV Project OPERO. 62. Deutscher Luft- und Raumfahrt Kongress 2013, 10-12 September 2013, Stuttgart, Deutschland. Volltext nicht frei.
Marquez Gutierrez, Carlos Omar and Stürmer, Arne and Clemen, Carsten (2011) Installation Effects of a CROR Propulsion System on a Modified DLR-F6 Aircraft Configuration. 20th International Society of Airbreathing Engines Conference, 12-16 September 2011, Göteborg, Schweden. Volltext nicht frei.
Marquez Gutierrez, Carlos Omar and Stürmer, Arne and Clemen, Carsten and Grimminger, Andreas (2012) Validation of Actuator Disk Simulations of CROR Propulsion Systems at Low-Speed Flight Conditions. 30th AIAA Applied Aerodynamics Conference, 25.-28. Juni 2012, New Orleans, LA, USA. Volltext nicht frei.
Meissner, Dietmar and Cusset, Francois and Wild, Jochen and Schulz, Matthias (2013) Experimental Verification of the DESIREH High-Lift Wing at Aircraft Flight Conditions. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 1.-4. Juli 2013, München, Deutschland. Volltext nicht online.
Melber-Wilkending, Stefan (2008) Application of Advanced CFD Tools for Cryogenic Testing. 5th. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2008), 2008-06-30 - 2008-07-04, Venice. (Unpublished) Volltext nicht online.
Melber-Wilkending, Stefan and Bergmann, Andreas (2012) Aeroacoustic optimization of the NWB airline and turning vanes based on high fidelity CFD and acoustic simulation. 18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, USA. Volltext nicht frei.
Melber-Wilkending, Stefan (2008) Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-lift Configuration. 16th AG STAB/DGLR Symposium, 2008-11-03 - 2008-11-04, Aachen.
Melber-Wilkending, Stefan (2014) Numerische Untersuchung aerodynamischer Effekte im Flügelrumpfübergang einer Hochauftriebskonfiguration. Dissertation. DLR-Forschungsbericht. DLR-FB 2014-21, 136 S. Volltext nicht online.
Melber-Wilkending, Stefan (2003) Near field CFD calculations of baseline configuration. Project Report. Volltext nicht online.
Melber-Wilkending, Stefan (2004) Near field CFD calculations for variations on baseline configuration. Project Report. Volltext nicht online.
Melber-Wilkending, Stefan (2005) RANS-Solutions of complex configurations as Input for Vortex-Rollup Studies, Part III. Project Report. Volltext nicht online.
Melber-Wilkending, Stefan (2005) Synthesis of near field CFD calculations of DLR. Project Report. Volltext nicht online.
Melber-Wilkending, Stefan and Allen, S. and Breitsamter, C. (2007) A Comparision between CFD and Wind Tunnel Measurements for Wake Vortex Prediction. First CEAS European Air and Space Conference, 10.-13. September 2007, Berlin, Deutschland. Volltext nicht online.
Melber-Wilkending, Stefan and Wichmann, Georg (2008) Application of Advanced CFD Tools for High Reynolds Number Testing. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 2009-01-05 - 2009-01-08, Orlando, Florida.
Meyer, Michael and Lengers, Matthias and Bieler, Heribert and Fricke, Sebastian and Wild, Jochen and Norman, David (2014) Designing and Testing Active Flow Control Systems at the Junction of Ultra-High Bypass Ratio Engines and the Wing. 6th European Conference on Computational Fluid Dynamics, 20.-25. Jul. 2014, Barcelona, Spanien.
Nallapula, Varun and Bier, Niko and Rohlmann, David and Radespiel, Rolf (2012) Simulation of the Horizontal Tail Plane Stall of a Transport Aircraft. 42nd AIAA Fluid Dynamics Conference and Exhibit, 25.-28. Jun. 2012, New Orleans, Louisiana, USA. Volltext nicht online.
Neitzke, Klaus-Peter and Rudnik, Ralf and Schröder, Andreas (2005) Low Speed Validation Tests on Engine/Airframe Integration within the European Project EUROLIFT II. 41st AIAA Joint Propulsion Conference, 2005-07-23 - 2005-07-26, Tucson, Arizona (USA). ISBN 978-1-56347-764-5 Volltext nicht online.
Ohira, Keisuke and Kwak, Dongyoun and Brezillon, Joël and Gaffuri, Michele (2012) Numerical Study of the Eddy Viscosity Turbulence Model for High Alpha Flow over the Low Aspect Ratio Wing. 44th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2012, 5-6 Jul 2012, Toyama, Japan. Volltext nicht online.
Pallek, Dieter and von Geyr, Heiko and Schröder, Andreas (2008) Experimental and numerical study on the flow behind a TPS. 14th International Symposium on Application of Laser Techniques to Fluid Mechanics, 2008-07-07 - 2008-07-10, Lisbon (Portugal). Volltext nicht online.
Pinkowski, Andre and Lüdeke, Heinrich (2015) Direct numerical simulation of benchmark test cases by a spectral high order method. Other. DLR-Interner Bericht. DLR-IB 124-2015/3, 21 S. Volltext nicht frei.
Politz, Christina and Grüttemann, Andreas and Kreienfeld, Malte and Schröder, Andreas and Konrath, Robert and Boden, Fritz and Lawson, Nicholas and Casella, Domenico (2009) High lift flow structures: In-flight PIV feasibility study. AIM Final Workshop, 27.10.-28.10.2009, Göttingen, Germany. Volltext nicht online.
Quix, Harald and Schulz, Matthias and Quest, Jürgen and Rudnik, Ralf and Schröder, Andreas (2007) Low Speed High Lift Validation Tests within the European Project EUROLIFT II. American Institute of Aeronautics and Astronautics. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL (USA). Volltext nicht online.
Rabe, Jens and Hepperle, Martin (2015) Title confidential. DLR-Interner Bericht. DLR-IB 124-2015/908, 27 S. Volltext nicht online.
Radespiel, Rolf and Haucke, Frank and Kähler, C. and Messing, R. and Nitsche, Wolfgang and Peltzer, Inken and Rist, U. and Scholz, Peter and Wichmann, Georg and Wild, Jochen and Gölling, Burkhard (2009) Dynamic Flow Control Experiments for Innovative High-Lift Configurations on IHK/M-FLY Programs. KATnet II Conference on Key Aerodynamics Technologies, 12.-14. Mai 2009, Bremen, Germany. Volltext nicht frei.
Riedel, H. (2016) Die Massenerhaltungsgleichung und die Bewegungsgleichungen für Kontinuumströmung. DLR-Interner Bericht. DLR-IB-AS-BS-2016-10, 182 S. Volltext nicht online.
Riedel, H. and Sitzmann, M. (2015) Application of the eN method of linear boundary layer stability theory to a natural laminar flow engine nacelle. DLR-Interner Bericht. DLR-IB 124-2015/1, 45 S. Volltext nicht online.
Risse, Kristof and Stumpf, Eike (2016) Integrated Design Method for Aircraft with Hybrid Laminar Flow Control Wings. 7th European Congress on Computational Methods in Applied Sciences and Engineering 2016, 5.-10. Juni 2016, Hersonissos, Griechenland. Volltext nicht online.
Ritter, Sebastian (2013) Untersuchung des Einflusses der Position eines eng gekoppelten Ultra-High-Bypass-Triebwerks auf eine Hochauftriebskonfiguration. In: Jahresbericht 2013, 2013, pp. 24-25. 16. STAB-Workshop, 12.-13. Nov. 2013, Göttingen, Deutschland.
Ritter, Sebastian (2014) Impact of different UHBR-Engine positions on the aerodynamics of a high-lift-wing. Symposium "Simulation of Wing and Nacelle Stall", 01.-02. Dez. 2014, Braunschweig. Volltext nicht online.
Rivers, Melissa and Quest, Juergen and Rudnik, Ralf (2015) Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited). SciTech 2015, 05.-09. Jan. 2015, Kissimmee, USA.
Rohardt, Claas-Hinrik (2012) Ermittlung des Grenz-NTS-Faktors im NWB-DNW. DLR-Interner Bericht. DLR-IB 124-2012/913, 66 S. Volltext nicht frei.
Rohardt, Claas-Hinrik and Küpper, Albert (2014) Determination of the NTS-factor for the DNW-NWB. 19. DGLR-Fach-Symposium der STAB, 4.-5. November 2014, München. Volltext nicht frei.
Rohlmann, David (2014) Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration. Joint Symposium of DFG FOR 1066 and DLR-Airbus C2A2S2E: "Simulation of Wing and Nacelle Stall", 01.-02. Dez. 2014, Braunschweig, Deutschland. Volltext nicht online.
Rohlmann, David (2015) Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration. In: Advances in Simulation of Wing and Nacelle Stall Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), 131. Springer International Publishing. pp. 381-395. ISBN 978-3-319-21126-8. ISSN 1612-2909 Volltext nicht online.
Rohlmann, David (2016) Numerische Simulation des Einflusses des Fahrwerks und des Bodeneffekts auf die Umströmung einer Transportflugzeugkonfiguration. Deutscher Luft- und Raumfahrtkongress 2016, 13.-15.09.2016, Braunschweig, Deutschland. Volltext nicht online.
Rohlmann, David and Keye, Stefan (2015) Stall Maneuver Simulation of an elastic Transport Aircraft based on Flight Test Data. 33rd AIAA Applied Aerodynamics Conference, 22.-26. Juni 2015, Dallas, USA. Volltext nicht online.
Ronzheimer, Arno and Hepperle, Martin and Brezillon, Joël and Brodersen, Olaf and Lieser, Jan (2013) Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet Configuration. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 121. Springer Verlag. pp. 25-32. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.
Ronzheimer, Arno (2006) Prospects of Geometry Parameterization based on Freeform Deformation in MDO. In: ERCOFTAC 2006: Design Optimisation: Methods & Applications, pp. 1-10. ERCOFTAC 2006 International Conference, [2006-04-05 - 2006-04-07], Las Palmas de Gran Canaria, Spain. ISBN 84-85650-12-3 Volltext nicht frei.
Ronzheimer, Arno (2010) Investigation and Minimization of Upsweep Drag of Aft-Loading Military Transporters with Tail Strakes. 28th AIAA Applied Aerodynamics Conference, 28 June - 1 July 2010, Chicago, Illinois. Volltext nicht frei.
Ronzheimer, Arno (2012) Aircraft Geometry Parameterization with High-End CAD-Software for Design Optimization. ECCOMAS 2012, 10.-14. September 2012, Wien, Östereich. ISBN 978-3-9502481-9-7 Volltext nicht frei.
Ronzheimer, Arno and Brezillon, Joel and Brodersen, Olaf (2010) Aerodynamisch optimale Triebwerksintegration am Heck einer generischen Geschäftsreiseflugzeugkonfiguration. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.
Ronzheimer, Arno and Hepperle, Martin and Brezillon, Joël and Lieser, Jan (2012) Aerodynamic Optimal Engine Integration for a Business Jet Configuration. 8th AIAA Multidisciplinary Design Optimization Specialist Conference (MDO), 23.-26. April 2012, Honolulu, Hawaii. ISBN 978-1-60086-937-2 Volltext nicht frei.
Ronzheimer, Arno and Natterer, Franz Josef and Brezillon, Joël (2010) Aircraft Wing Optimization Using High Fidelity Closely Coupled CFD and CSM Methods. 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, Fort Worth, Texas, Fort Worth, Texas. Volltext nicht frei.
Roosenboom, Eric and Schröder, Andreas and Geisler, Reinhard and Pallek, Dieter and Agocs, Janos and Stürmer, Arne and Marquez Gutierrez, Carlos Omar and Neitzke, Klaus-Peter (2011) Experimental and numerical investigation of a counter rotating open rotor flow field. 29th AIAA Applied Aerodynamics Conference, 27.-30. Jun. 2011 , Honolulu, Hawaii, USA. Volltext nicht online.
Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2009) Comparison of PIV measurements with unsteady RANS calculations in a propeller slipstream. 27th AIAA Applied Aerodynamics Conference, 22 - 25 June 2009, San Antonio, Texas, USA. ISBN 978-1-56347-975-5 Volltext nicht online.
Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2010) Advanced Experimental and Numerical Validation and Analysis of Propeller Slipstream Flows. Journal of Aircraft, Vol. 47 (1), pp. 284-291. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.45961 ISSN 0021-8669 Volltext nicht online.
Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2011) PIV data for numerical validation - Application to propeller flow fields -. CFD and Experiment – Integration of Simulation, Workshop of the DGLR-Querschnittsbereich Thermo- and Fluiddynamics, 05. - 06. Apr. 2011, Göttingen, Deutschland. Volltext nicht online.
Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2008) Comparison of uRANS CFD calculation with phase-locked PIV measurement data for propeller flow. EWA - PIV/CFD Joint Workshop, 2008-09-23 - 2008-09-24, Modane (France). Volltext nicht online.
Rudnik, R. and Melber-Wilkending, Stefan and Huber, Kerstin Claudie and Crippa, Simone (2016) DLR`s Contributions to the AIAA High Lift Prediction Workshop Series to conclusions. Deutscher Luft- und Raumfahrtkongress 2016, 13.-15. Sep. 2016, Braunschweig, Deutschland. DOI: urn:nbn:de:101:1-20160903771 Volltext nicht online.
Rudnik, R. and Schwetzler, Detlev (2016) High lift INflight Validation (HINVA) - Overview about the 2nd Flight Test Campaign. In: AIAA 54nd Aerospace Sciences Meeting. SciTech 2016, 04.-08. Jan. 2016, San Diego, USA. DOI: AIAA 2016-0041 Volltext nicht online.
Rudnik, Ralf (2014) Konfigurationsaerodynamik. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag GmbH & Co. KG. pp. 83-113. ISBN 978-3446423411. Volltext nicht online.
Rudnik, Ralf and Bier, Niko and Quest, Jürgen and Schulz, Matthias (2015) Flight Test Tailored ETW Testing of a Commercial Transport High Lift Configuration. 53rd AIAA Aerospace Sciences Meeting, 5.-9. January 2015, Kissimmee (FL), USA. DOI: [10.2514/6.2015-1559] Volltext nicht online.
Rudnik, Ralf and Huber, Kerstin Claudie and Melber-Wilkending, Stefan (2012) EUROLIFT Test Case Description for the 2nd High Lift Prediction Workshop. 30th AIAA Applied Aerodynamics Conference, 25.-28. Juni 2012, New Orleans. Volltext nicht online.
Rudnik, Ralf and Melber-Wilkending, Stefan (2014) DLR Contribution to the 2nd High Lift Prediction Workshop. SciTech 2014, 13.-17. Jan. 2014, National Harbor, USA. Volltext nicht online.
Rudnik, Ralf and Melber-Wilkending, Stefan (2013) DLR Contribution to the Second High Lift Prediction Workshop. 31st AIAA Applied Aeordynamics Conference, 24.-27. Juni 2013, San Diego, USA. Volltext nicht online.
Rudnik, Ralf and Reckzeh, Daniel and Quest, Juergen (2012) HINVA - High Lift INflight VAlidation - Project Overview and Status. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 09.-12. Jan. 2012, Nashville, USA. Volltext nicht online.
Rudnik, Ralf and Schwetzler, Detlev (2014) High lift INflight VAlidation (HINVA) - Overview about the 1st Flight Test Campaign. 32nd AIAA Applied Aerodynamics Conference, 16.-20. Juni 2014, Atlanta, USA. Volltext nicht online.
Savoni, Luciana and Rudnik, Ralf (2016) Aerodynamic Assessment of Pylon-Mounted Over-the-wing Engine Installations on a STOL Commercial Aircraft Concept. 20. DGLR-Fach-Symposium der STAB, 8-9 November 2016, Braunschweig. Volltext nicht online.
Schade, Niko (2010) Simulation of Store Separation - Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations. 17. DGLR-Fach Symposium der STAB, Berlin, Germany. Volltext nicht online.
Schade, Niko (2013) Simulation of Store Separation - Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations. In: New Results in Numerical and Experimental Fluid Mechanics VIII New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 17-24. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.
Schmid, Sven and Lutz, Thorsten and Krämer, Ewald and Kühn, Timo (2009) Passive Control of the Flow Around the Stratospheric Observatory for Infrared Astronomy. Journal of Aircraft, 46 (4), pp. 1319-1325. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.40777 Volltext nicht online.
Schmidt, Stephan and Gauger, Nicolas and Ilic, Caslav and Schulz, Volker (2011) Three dimensional large scale aerodynamic shape optimization based on shape calculus. 41st AIAA Fluid Dynamics Conference and Exhibit, June 27-30, 2011, Honolulu, USA.
Scholz, Peter and Kähler, Christian and Radespiel, Rolf and Wild, Jochen and Wichmann, Georg (2009) Active Control of Leading-Edge Separation within the German Flow Control Network. In: 47th AIAA Aerospace Sciences Meeting (AIAA 2009-0529). AIAA. ASM 2009, 2009-01-05 - 2009-01-08, Orlando, FL (USA). Volltext nicht online.
Schröder, Andreas and Pallek, Dieter and Geisler, Reinhard and Lauke, Thomas and Herr, Michela and Geyr, Heiko v. and Dierksheide, Uwe (2009) Particle Image Velocimetry as Validation Tool in Aeronautics. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 2009-01-05 - 2009-01-08, Orlando, FL (USA). Volltext nicht online.
Schröder, Andreas and Agocs, Janos and Geisler, Reinhard and Heider, André and Konrath, Robert and Pallek, Dieter and Roosenboom, Eric and von Geyr, Heiko and Stürmer, Arne (2008) Particle Image Velocimetry as Validation Tool in Aeronautics. Artes Gráficas Torres S.L., Morales 17, 08029 Barcelona, Spain. 5th. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2008), 2008-06-30 - 2008-07-04, Venice (Italy). ISBN 978-84-96736-55-9 Volltext nicht online.
Schröder, Andreas and Göing, Markus and Pallek, Dieter and Geyr, Heiko v. (2007) Experimental and numerical characterisation of the flow behind a TPS. Joint EWA and UFAST Workshop on Validation of Numerical Methods by Experiments in Aerodynamics, 2007-06-04 -2007-06-06, Prag (Tschechischen Republik). Volltext nicht online.
Schütte, A. and Boelens, O.J. and Löser, T. and Oehlke, M. (2010) Prediction of the Flow Around the X-31 Aircraft Using Two Different CFD Methods. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 01. Juli 2010, Chicago, USA. Volltext nicht online.
Schütte, Andreas and Boelens, Okko J. and Oehlke, Martin and Jirásek, Adam and Loeser, Thomas (2012) Prediction of the flow around the X-31 aircraft using three different CFD methods. Aerospace Science and Technology, 20 (1), pp. 21-37. Elsevier. DOI: doi:10.1016/j.ast.2011.07.014 ISSN 1270-9638 Volltext nicht online.
Schütte, Andreas and Cummings, Russ M. and Loeser, Thomas (2012) An integrated computational/experimental approach to X-31 stability & control estimation. Aerospace Science and Technology, 20 (1), pp. 2-11. Elsevier. DOI: 10.1016/j.ast.2011.10.010 ISSN 1270-9638 Volltext nicht online.
Schütte, Andreas and Hummel, D. and Hitzel, S. (2010) Numerical and Experimental Analyses of the Vortical Flow Around the SACCON Configuration. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 1. Juli 2010, Chicago, USA. Volltext nicht online.
Schütte, Andreas and Hummel, Dietrich and Hitzel, Stephan M. (2012) Flow Physics Analyses of a Generic Unmanned Combat Aerial Vehicle Configuration. Journal of Aircraft, 49 (6), pp. 1638-1651. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C031386 ISSN 0021-8669 Volltext nicht online.
Schütte, Andreas and Lüdeke, Heinrich (2013) Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code. Aerospace Science and Technology, 24 (1), pp. 56-65. Elsevier. DOI: [10.1016/j.ast.2012.03.002] ISSN 1270-9638 Volltext nicht online.
Schütte, Andreas (2016) Numerical investigations of the vortical flow on swept wings with round leading edges. 34th AIAA Applied Aerodynamics Conference, 13.-17. Juni 2016, Washington DC, USA. DOI: 10.2514/6.2016-4172 Volltext nicht frei.
Schütte, Andreas and Huber, Kerstin Claudie and Boelens, Okko J. (2014) Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices. In: 32nd AIAA Applied Aerodynamics Conference (2132), pp. 1-26. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, USA.
Schütte, Andreas and Lüdeke, Heinrich (2008) Numerical investigations on the VFE-2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, Nevada, USA. Volltext nicht frei.
Seitz, Arne (2008) Recent Drag Reduction Activities at DLR. Drag Reduction Workshop 4, 14.-16. Oktober 2008, Ascot, United Kingdom. Volltext nicht online.
Seitz, Arne (2012) Rekonstruktion eines Störströmungsfeldes aus der Wandmessung von Tollmien-Schlichting Wellen. 18. DGLR-Facg-Symposium der STAB, 06. - 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online.
Seitz, Arne and Horstmann, Karl-Heinz (2010) Design Studies on NLF and HLFC Applications at DLR. International Council of the Aeronautical Sciences. ICAS 2010, 19.-24. September 2010, Nizza, Frankreich. ISBN 978-0-9565333-0-2 Volltext nicht frei.
Seitz, Arne (2014) Reconstruction of a Disturbance Flow Field from Wall Measurements of Tollmien-Schlichting Waves. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag. pp. 203-211. ISBN 978 3 319 03157 6. ISSN 1612-2909 Volltext nicht frei.
Streit, Thomas and Hoffrogge, Cornelius (2016) Erweiterung des 3D inversen Verfahrens auf Randbedingungen mit 2 Symmetrieebenen. DLR-Interner Bericht. DLR-IB-AS-BS-2016-95, 34 S. Volltext nicht online.
Streit, Thomas and Hoffrogge, Cornelius (2016) DLR TRANSONIC INVERSE DESIGN CODE, EXTENSIONS AND MODIFICATIONS TO INCREASE VERSATILITY AND ROBUSTNESS. RAeS 2016 Appllied Aerodynamics Conference, 18-21 Jul. 2016, Bristol, United Kingdom. Volltext nicht online.
Streit, Thomas and Wedler, Sven and Kruse, Martin (2014) DLR NATURAL AND HYBRID TRANSONIC LAMINAR WING DESIGN INCORPORATING NEW METHODOLOGIES. RAeS Advanced Aero Concepts, Design and Operations Conference, 22 – 24 Jul. 2014, Bristol, United Kingdom. Volltext nicht online.
Streit, Thomas and Horstmann, Karl Heinz and Schrauf, Géza and Hein, Stefan and Fey, Uwe and Egami, Yasuhiro and Perraud, Jean and Salah El Din, Itham and Cella, Ubaldo and Quest, Jürgen (2011) Complementary Numerical and Experimental Data Analysis of the ETW Telfona Pathfinder Wing Transition Tests. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 4 - 7 January 2011, Orlando, Florida USA. Volltext nicht frei.
Streit, Thomas and Wichmann, Georg and von Knoblauch zu Hatzbach, Fedime and Campbell, Richard L. (2011) Implications of Conical Flow for Laminar Wing Design and Analysis. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, Hawaii, USA. Volltext nicht frei.
Strüber, Henning and Wild, Jochen (2014) Aerodynamic Design of a High-Lift System Compatible with a Natural Laminar Flow Wing within the DeSiReH Project. In: ICAS 2014 CD-Rom Proceedings, e300. 29th Congress of the International Council of the Aeronautical Sciences, 7.-12. Sep. 2014, St. Petersburg, Russia. ISBN 3-932182-80-4 Volltext nicht frei.
Stürmer, Arne (2007) Unsteady Simulations of a Generic Isolated Tractor Contra-Rotating Propeller with the DLR TAU-Code. DLR-Interner Bericht. DLR-IB 124-2007/913, 41 S. Volltext nicht online.
Stürmer, Arne (2007) CFD Validation of Unsteady Installed Propeller Flows Using the DLR TAU-Code. DGLR. 1st CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin, Deutschland. ISSN 0070-4083 Volltext nicht online.
Stürmer, Arne (2006) Unsteady CFD Simulations of Propeller Installation Effects. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006-07-09 - 2006-07-12, Sacramento, CA (USA). Volltext nicht online.
Stürmer, Arne (2008) Unsteady CFD Simulations of Contra-Rotating Propeller Propulsion Systems. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2008-07-21 - 2008-07-23, Hartford, CT, USA. Volltext nicht online.
Stürmer, Arne and Marquez Gutierrez, Carlos Omar and Roosenboom, Eric and Schröder, Andreas and Geisler, Reinhard and Pallek, Dieter and Agocs, Janos and Neitzke, Klaus-Peter (2012) Experimental and Numerical Investigation of a Contra Rotating Open-Rotor Flowfield. Journal of Aircraft, Vol. 49 (6), pp. 1868-1877. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C031698 ISSN 0021-8669 Volltext nicht online.
Stürmer, Arne (2010) Multi-Disciplinary Numerical Analysis for the Contra-Rotating Open Rotor. MUSAF Colloquium, 27-29 Sep 2010, Toulouse, France. (Unpublished) Volltext nicht online.
Stürmer, Arne (2010) Numerical Analysis of CROR Propulsion System Aerodynamics and Aeroacoustics at DLR. 2nd UTIAS-MITACS International Workshop on Aviation and Climate Change, 27-28 May 2010, Toronto, Canada. (Unpublished) Volltext nicht online.
Stürmer, Arne (2010) DLR CROR & Propeller Noise Prediction: Numerical Approach Requirements & Limitations. 14th CEAS-ASC Workshop, 7-8 Oct 2010, Warsaw, Poland. (Unpublished) Volltext nicht online.
Stürmer, Arne (2015) Validation of Installation Effect Predictions Through Simulations of Contra-Rotating Open Rotors at Low-Speed Flight Conditions. In: AIAA Aviation 2015. AIAA Aviation 2015, 22.-26.06.2015, Dallas, TX, USA. Volltext nicht online.
Stürmer, Arne and Yin, Jianping (2010) Active Control of Unsteady Blade Loads for Installed CROR Propulsion Systems. 17. DGLR-Fach Symposium der STAB, 9-10 Nov 2010, Berlin, Germany. (Unpublished) Volltext nicht online.
Tinoco, Edward and Brodersen, Olaf and Keye, Stefan and Laflin, Kelly and Feltrop, Edward and Vassberg, John and Mani, Mori and Rider, Ben and Wahls, Richard and Morrison, Joseph and Hue, David and Gariepy, Martin and Roy, Christopher and Mavriplis, Dimitri and Murayama, Mitsuhiro (2017) Summary of Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases 2 to 5. In: AIAA 2017-1208. AIAA Science and Technology Forum and Exhibition (SciTech), 9.-13. Jan. 2017, Grapevine, USA. Volltext nicht online.
Vicroy, Dan D. and Loeser, Thomas D. and Schütte, Andreas (2012) Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle. Journal of Aircraft, 49 (6), pp. 1558-1583. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C031501 ISSN 0021-8669 Volltext nicht online.
Vicroy, Dan D. and Huber, Kerstin Claudie and Rohlf, Detlef and Löser, Thomas (2014) Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls. In: 32nd AIAA Applied Aerodynamics Conference (2003), pp. 1-24. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA. Volltext nicht online.
Vollmers, Heinrich and Puffert-Meissner, Wolfgang and Schröder, Andreas (2005) Analysis of PIV Flow Field Measurements behind the ALVAST-Model in High-Lift Configuration. In: Springer-Verlag Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), Vol. 92. Springer. pp. 17-24. ISBN 3-540-33286-3. Volltext nicht online.
Vormweg, Jan (2016) Aerodynamische Entwurfsstudien und Analysen der Strömungsphysik an einer Nurflügelkonfiguration. Diploma. DLR-Interner Bericht. DLR-IB-AS-BS-2016-185, 87 S.
Voss, Guido and Gerz, Thomas and Baumann, Robert and Stumpf, Eike and Press, Michael (2009) Wake Vortex Alleviation by Differential and Oscillating Flap Setting: A flight test. 27th Applied Aerodynamics Conference, 22-25 Jun 2009, San Antonio, Texas.
Voß, Guido and Carmer, Carl F. v. and Konrath, Robert and Stumpf, Eike and Krückeberg, Claus-Peter and Meyer, Hans-Henning and Mattner, Hartmut (2007) Wake vortex alleviation by differential and oscillating flap setting: a comparative numerical and experimental study. 1st CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin. ISSN 0700-4083 Volltext nicht online.
v. Geyr, Heiko and Schade, Niko (2010) Prediction of Maximum Lift Effects on Realistic High-Lift-Commercial-Aircraft-Configurations within the European project EUROLIFT II. Second Symposium "Simulation of Wing and Nacelle Stall", June 22nd - 23rd, 2010, Braunschweig. Volltext nicht online.
v. Geyr, Judith and v. Knoblauch z. Hatzbach, Fedime and Arne, Seitz and Thomas, Streit and Georg, Wichmann (2012) Wing Design based on a Tapered Wing NLF Airfoil Catalogue. 18. DGLR-Fach-Symposium der STAB, 06. - 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online.
Wedler, Sven (2015) Analysis Regarding Variable Cambering with Spoiler Tracking: Effect of the Flap Hinge Line Location on the Aerodynamic at Transonic Speeds. 64. Deutscher Luft- und Raumfahrtkongress, 22-24 Sep 2015, Rostock, Germany. Volltext nicht frei.
Wedler, Sven and Seitz, Arne (2014) Specifications of HLFC Devices for Flight Test Applications. DLR-Interner Bericht. DLR-IB 124-2014/905, 34 S. Volltext nicht online.
Wedler, Sven and Streit, Thomas (2014) New Methodologies Tailored for the design of Aerodynamically Robust Laminar Wings. Greener Aviation: Clean Sky breakthroughs and worldwide status, 12. - 14. Mrz., Brüssel, Belgien. Volltext nicht frei.
Wichmann, Georg (2017) Transsonische Profil- und Tragflügelentwicklung am Institut für Aerodynamik und Strömungstechnik. DLR-Interner Bericht. DLR-IB-AS-BS-2017-32, 90 S. Volltext nicht frei.
Wicke, Kai and Kruse, Martin and Linke, Florian and Gollnick, Volker (2015) Insect Contamination Impact on Operational and Economic Effectiveness of Natural-Laminar-Flow Aircraft. Journal of Aircraft. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C033237 ISSN 0021-8669 Volltext nicht frei.
Wild, Jochen (2008) Multi-objective constrained optimisation in aerodynamic design of high-lift systems. International Journal of Computational Fluid Dynamics, 22 (3), pp. 153-168. Taylor & Francis. DOI: 10.1080/10618560701868420 ISSN 1061-8562 Volltext nicht online.
Wild, Jochen (2008) Active Separation Control on the Leading Edge of a Slatless Swept Wing in High Lift Configuration Using Steady Blowing in the European Project EUROLIFT II. KATNet II Separation Control Workshop, 2008-04-01 - 2008-04-03, Toulouse. Volltext nicht online.
Wild, Jochen and Brezillon, Joel (2008) Optimization of 3-D Multi-Element High-Lift Device Configuration. In: 5th. European Congress on Computational Methods in Applied Sciences and Engineering. ECCOMAS 2008, 2008-06-30 - 2008-07-05, Venedig, IT. Volltext nicht online.
Wild, Jochen and Brezillon, Joel and Amoignon, Olivier and Quest, Jürgen and Moens, Frederic and Quagliarella, Domenico (2009) Advanced Design by Numerical Methods and Wind Tunnel Verification within the European High-Lift Program. Journal of Aircraft, 46 (1), pp. 157-167. American Institute of Aeronautics and Astronautics (AIAA). ISSN 0021-8669 Volltext nicht online.
Wild, Jochen and Brezillon, Joel and Mertins, Ralf and Quagliarella, Domenico and Germain, Eric and Amoignon, Olivier and Moens, Frederic (2006) REALISTIC HIGH-LIFT DESIGN OF TRANSPORT AIRCRAFT BY APPLYING NUMERICAL OPTIMIZATION. In: ECCOMAS CFD 2006. ECCOMAS CFD 2006, 2006-09-05 - 2006-09-08, Egmond aan Zee, NL. Volltext nicht online.
Wild, Jochen and Dettmar, Holger (2006) Beeinflussung der Anlegelinie-Transition am Vorflügel durch Geometriemodifikationen. 15. DGLR Fachsymposium der STAB, 2006-11-29 - 2006-12-01, Darmstadt. Volltext nicht online.
Wild, Jochen and Dettmar, Holger (2007) Manipulation of Attachment Line Transition by Geometry Modification at the Slat of a Multi-Element Airfoil. Springer. 15th STAB/DGLR Symposium, 2006-11-29 - 2006-12-01, Darmstadt. ISBN 3-540-74458-4 Volltext nicht online.
Wild, Jochen and Haucke, Frank and Scholz, Peter (2008) Large scale separation flow control experiments within the German Flow Control Network. KATNet II Separation Control Workshop, 2008-04-01 - 2008-04-03, Toulouse. Volltext nicht online.
Wild, Jochen (2011) Smooth Mixed Meshes for Acceleration of RANS CFD in Aircraft Analysis and Design. 49th AIAA Aerospace Sciences Meeting, 4.-7. Jan. 2011, Orlando, FL, USA.
Wild, Jochen (2012) Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3-element high-lift wing sections. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 9.-12. Jan. 2012, Nashville, TN, USA.
Wild, Jochen (2012) Quality assessment of Smooth Block-Unstructured Mixed Meshes for Aerodynamic Applications. MASCOT/ISGG 2012, 22.-26. Okt. 2012, Las Palmas de Gran Canaria, Spain.
Wild, Jochen (2013) Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections. Journal of Aircraft, 50 (4), pp. 1202-1216. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C032138 ISSN 0021-8669 Volltext nicht online.
Wild, Jochen (2013) Overview on the DeSiReH Project. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 1.-4. Juli 2013, München, Deutschland.
Wild, Jochen (2014) Quality Assessment of Smooth Block-Unstructured Mixed Meshes for Aerodynamic Applications. In: MASCOT 12 & ISGG 12 IMACS Series in Computational and Applied Mathematics, 18. IMACS International Association for Mathematics and Computers in Simulation. pp. 291-300. ISSN 1098-870X Volltext nicht online.
Wild, Jochen (2014) Mach-, Reynolds- and Sweep Effects on Active Flow Separation Control Effectivity on a 2-Element Airfoil Wing. In: Acitve Flow and Combustion Control 2014 Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 127. Springer Verlag. pp. 87-100. ISBN 978-3-319-11966-3. ISSN 1612-2909 Volltext nicht online.
Wild, Jochen (2014) Simulation and Flight Re-Number Testing of High-Lift Systems. 6th European Conference on Computational Fluid Dynamics, 20.-25. Jul. 2014, Barcelona, Spanien.
Wild, Jochen (2014) Hochauftrieb. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag München. pp. 184-192. ISBN ISBN 978-3-446-42341-1. Volltext nicht online.
Wild, Jochen (2015) Recent Research Topics in High-lift Aerodynamics. Deutscher Luft- und Raumfahrtkongress (DLRK) 2015, 22.-24.09.2015, Rostock, Germany. Volltext nicht online.
Wild, Jochen (2015) High-Performance High-Lift Design for Laminar Wings. AeroDays 2015, 20.-23. Okt. 2015, London, United Kingdom. Volltext nicht online.
Wild, Jochen (2016) On the Most Common Misunderstandings of High-Lift Flows. AEROSPATIAL 2016, 26.-27. Okt. 2016, Bukarest, Rumänien.
Wild, Jochen and Franke, Dirk M. (2015) Krüger design for an HLFC wing. 5th CEAS Air & Space Conference (CEAS 2015), 07.-10. Sep. 2015, Delft, The Netherlands. Volltext nicht frei.
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Winkler, Michael and Huber, Kerstin Claudie (2016) Numerische Bewertung innovativer Steuerflächen einer generischen Lamdaflügelkonfiguration. Master's. DLR-Interner Bericht. EB 124-2016/901, 110 S. Volltext nicht online.
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