Items where Subject is "German-Dutch Windtunnels"

Beaumier, Philippe and van der Wall, Berend G. and Keßler, Christoph and Delrieux, Yves and Gervais, Marc and Hirsch, Jean-Francois and Pengel, Kurt and Crozier, Pascal (2016) From ERATO Basic Research to the Blue Edge Rotor Blade: an Example of Virtual Engineering? Rotorcraft Virtual Engineering Conference, 2016-11-08 - 2016-11-10, Liverpool. Volltext nicht online.

Beck, Walter and Henne, Ulrich and Hirschen, Christian (2013) Application of the Pressure Sensitive Paint (PSP) Technique to a Scramjet Nozzle Flow in the DLR Hypersonic Wind Tunnel H2K. Seminar China Academy of Aerospace Aerodynamics (CAAA), 2013-08-13, Beijing, P.R. China. Volltext nicht online.

Bock, K.-W. and Rebstock, Rüdiger and Zhai, Junnai and Klein, Christian and Bruse, Martin (2013) Vorstellung DNW/DLR bei Fraunhofer LBF. Vorstellung Präsentation DNW / Problemstellung und Besichtigung des beheizten Windkanalmodells, 2013-03-12, Darmstadt, Deutschland. Volltext nicht online.

Bruse, Martin and Klein, Christian and Henne, Ulrich and Sachs, Werner (2010) DLR - AEDC combined wind tunnel test on PSP Intensity and Lifetime method. DEA-7425 Meeting, 2010-11-08 - 2010-11-09, Tennessee, USA. Volltext nicht online.

Burley, Casey L. and Brooks, Thomas F. and van der Wall, Berend G. and Richard, Hugues and Raffel, Markus and Beaumier, Philippe and Delrieux, Yves and Lim, Joon W. and Yu, Jung H. and Tung, Chee and Pengel, Kurt and Mercker, Edzard (2003) Rotor Wake Vortex Definition using 3C-PIV Measurements - Corrected for Vortex Orientation. 9th AIAA/CEAS Aeroacoustics Conference, 2003-05-12 - 2003-05-14, Hilton Head, SC (USA). Volltext nicht online.

Ciobaca, Vlad and Melber-Wilkending, Stefan and Wichmann, Georg and Bergmann, Andreas and Küpper, Albert (2012) Experimental and numerical studies of the low speed wind tunnel DNW-NWB’s open test section towards an aeroacoustic facility. In: AIAA Paper 2012-2174. 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), , 2012-06-04 - 2012-06-06, Colorado Springs, Colorado . doi: 10.2514/6.2012-2174. Volltext nicht frei.

Ciobaca, vlad and Pott-Pollenske, Stephan-Michael and Melber-Wilkending, Stefan and Wichmann, Georg (2012) Computational and Experimental Results in the Open Test Section of the Aeroacustic Windtunnel Braunschweig. Volltext nicht online.

Ciobaca, Vlad and Melber-Wilkending, Stefan and Pott-Pollenske, Michael (2009) A CFD process chain for simulating open windtunnel test sections. www.machtwissen.de AG. ISBN 978-3-00-027782-5.

Ciobaca, Vlad and Stefes, Bruno and de Bruin, Anton and Bauer, Matthias and Schlösser, Philipp and de Blecourt, Arnoud and Bier, Niko and Zhai, Junnai and Meyer, Michael and Wild, Jochen (2018) WIND TUNNEL EXPERIMENTS WITH LOCAL ACTIVE FLOW CONTROL FOR AIRCRAFT TOWARDS FUTURE FLIGHT TESTING. 31st Congress of the International Council of the Aerospace Sciences, 2018-09-09 - 2018-09-14, Belo Horizonte, Brasilien.

Cummings, Russel M. and Liersch, Carsten M. and Schütte, Andreas and Huber, Kerstin Claudie (2016) Aerodynamics and Conceptual Design Studies on an Unmanned Combat Aerial Vehicle Configuration. Journal of Aircraft, 55 (2), pp. 454-474. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C033808. ISSN 0021-8669. Volltext nicht frei.

Egami, Yasuhiro (2008) Title confidential. Project Report. HST-2008-XX. 10 S. (Submitted) Volltext nicht online.

Egami, Yasuhiro and Klein, Christian and Henne, Ulrich and Bruse, Martin and Ondrus, Valdimir and Beifuss, Uwe (2009) Development of a Highly Sensitive Temperature-Sensitive Paint for Measurements under Ambient (0 – 60 °C) Conditions. 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.

Egami, Yasuhiro and Klein, Christian and Henne, Ulrich and Fey, Uwe and Bruse, Martin and Ondrus, Valdimir and Beifuss, Uwe (2007) Title confidential. DLR-Interner Bericht. DLR-IB 224-2007 C 25. 21 S. Volltext nicht online.

Enders, Gerd (2009) Aerodynamische Inbetriebnahme des Verdichters des DNW-TWG, Phase 3. DLR-Interner Bericht. DLR-IB-325-16-09. DLR, Inst. für Antriebstechnik. 60 S. Volltext nicht online.

Geisbauer, Sven and Löser, Thomas (2017) Windkanalmessungen am DLR-F15DS Profil mit dynamischem Spoiler - Zusammenfassung der Messkampagne TN 2634. Project Report. DLR-EB 124-2017/905. 44 S. Volltext nicht frei.

Görtz, Stefan and Krumbein, Andreas and Ritter, Markus and Hofmann, Johannes (2018) DLR-Projekt VicToria - Virtual Aircraft Technology Integration Platform. Deutscher Luft- und Raumfahrtkongress 2018, 2018-09-04 - 2018-09-06, Friedrichshafen. Volltext nicht online.

Halle, Winfried and Schlicker, Martin (2007) Echtzeitbildverarbeitung zur Fernüberwachung von kleinen Flughäfen. 52. Internationales Kolloquium an der TU Ilmenau, 2007-09-10 - 2007-09-13, Ilmenau. Volltext nicht online.

Huber, Kerstin Claudie and Henne, Ulrich and Löser, Thomas and Schütte, Andreas (2017) Wind Tunnel Report TN2621: Static Force, Moment, Surface Pressure and PSP Measurements on the DLR-F19 Con-figuration including Spoiler Geometries and Control Surfaces. DLR-Interner Bericht. EB 124-2017/901. Other. DLR. 180 S. Volltext nicht online.

Huber, Kerstin Claudie and Loeser, Thomas and Looye, Gertjan and Liersch, Carsten M. and Lindermeir, Erwin and Kemptner, Erich and Klimmek, Thomas and Koch, Stefan and Kuchar, Richard and Nauroz, Mobin and Paul, Michael and Rein, Martin and Rode, Gerald and Rohlf, Detlef and Rütten, Markus and Schütte, Andreas and Schwithal, Jana and Siggel, Martin and Voss, Arne and Zimper, Dirk (2015) Bewertung und Entwurf von agilen und hoch gepfeilten Flugzeugkonfigurationen. DLR-Interner Bericht. DLR-IB 124-2015/913. 120 S. Volltext nicht online.

Huber, Kerstin Claudie and Schütte, Andreas and Rein, Martin and Löser, T. (2016) Experimental Aerodynamic Assessment and Evaluation of an Agile Highly Swept Aircraft Configuration. Deutscher Luft- und Raumfahrtkongress 2015, 2016-09-13 - 2016-09-15, Rostock, Deutschland. Volltext nicht online.

Huber, Kerstin Claudie and Schütte, Andreas and Rein, Martin and Löser, Thomas (2016) Experimental aerodynamic assessment and evaluation of an agile highly swept aircraft configuration. CEAS Aeronautical Journal, 8, pp. 17-29. Springer. doi: 10.1007/s13272-016-0219-y. ISSN 1869-5582. Volltext nicht frei.

Huber, Kerstin Claudie and Schütte, Andreas and Vicroy, Dan D. and Hübner, Andreas-René (2016) UCAV MODEL DESIGN AND STATIC EXPERIMENTAL INVESTIGATIONS TO ESTIMATE CONTROL DEVICE EFFECTIVENESS AND STABILITY AND CONTROL CAPABILITIES. NATO STO - Science and Technology Organisation. [Other] Volltext nicht online.

Huber, Kerstin Claudie and Vicroy, Dan D. and Schütte, Andreas and Hübner, Andreas-René (2014) UCAV model design and static experimental investigations to estimate control device effectiveness and Stability and Control capabilities. In: 32nd AIAA Applied Aerodynamics Conference (2002), pp. 1-21. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 2014-06-16 - 2014-06-20, Atlanta, GA, USA. doi: 10.2514/6.2014-2002.

Hübner, Andreas-René (2006) Experimental and numerical determination of dynamic derivatives of aircraft configuration. ONERA-DLR Aerospace Symposium, 2006-10-04 - 2006-10-06, Toulouse. Volltext nicht online.

Hübner, Andreas-René (2007) Experimental and numerical investigations of unsteady aerodynamic derivatives for transport aircraft configurations. In: AIAA Technical Conference. AIAA, 2007-01-09 - 2007-01-12, Reno, Nevada. Volltext nicht online.

Hübner, Andreas-René and Löser, Thomas (2005) Methods for determination of the unsteady aerodynamic derivatives for transport aircraft configurations. RTO-AVT-123, 2005-04-25 - 2005-04-29, Budapest. Volltext nicht online.

Jirásek, Adam and Cummings, Russel M. and Schütte, Andreas and Huber, Kerstin Claudie (2016) THE NATO STO AVT-201 SUMMARY. NATO STO - Science and Technology Organisation. [Other] Volltext nicht online.

Keye, Stefan (1991) Maßnahmen zur Verbesserung der Stabilität des Freistrahls in der offenen Meßstrecke des DNW-Modellkanals (PLST). Diploma, TU Clausthal. Volltext nicht online.

Klein, Christian and Bruse, Martin and Egami, Yasuhiro and Henne, Ulrich and Ondrus, Validimir and Beifuss, Uwe (2010) Development of a Highly Sensitive Temperature-Sensitive Paint (TSP) for Measurements at Ambient (0 – 60 °C) Conditions. DLR-ONERA MOTAR Meeting, 2010-03-29 - 2010-03-30, Saint Louis, France. Volltext nicht online.

Klein, Christian and Henne, Ulrich and Sachs, Werner and Beifuß, Uwe and Ondrus, Vladimir and Mai, Holger and Bruse, Martin (2010) Instationäre Druckmessung mittels Pressure-Sensitive Paint (PSP) am flexiblen Flügelmodell AEROSTABIL-A im DNW-TWG. 17. DGLR-Fach-Symposium der STAB, 2010-11-09 - 2010-11-10, Berlin, Deutschland. Volltext nicht online.

Klein , Christian and Beifuss, Uwe and Bruse, Martin and Egami, Yasuhiro and Henne, Ulrich and Ondrus, Vladimir (2010) Development of a Highly Sensitive Temperature-Sensitive Paint (TSP) for Measurements at Ambient (0 – 60 °C) Conditions. Seminar an China Aerodynamics Research and Development Center (CARDC), 2010-10-26, Mianyang, Sichuan, China. Volltext nicht online.

Kruse, Martin and Küpper, Albert and Petzold, Rouven and Munoz, Federico (2017) Determination of the Critical Cross Flow N-factor for the Low-Speed Wind Tunnel Braunschweig (DNW-NWB). In: New Results in Numerical and Experimental Fluid Mechanics XI, 136, pp. 251-261. Springer International Publishing. 20. DGLR/STAB Symposium, 2016-11-08 - 2016-11-09, Braunschweig, Deutschland. doi: 10.1007/978-3-319-64519-3_23. ISBN 978-3-319-64518-6. ISSN 1612-2909. Volltext nicht online.

Küfmann, Philip and Bartels, Rainer and van der Wall, Berend G. and Schneider, Oliver and Holthusen, Hermann and Gomes, Jorge and Postma, Jos (2016) The First Wind Tunnel Test of the DLR’s Multiple Swashplate System: Test Procedure and Preliminary Results. In: Proceedings of the 72nd Annual Forum of the American Helicoper Society. American Helicopter Society Inc.. 72nd AHS Forum, 2016-05-16 - 2016-05-19, West Palm Beach, USA. Volltext nicht online.

Küfmann, Philip and Bartels, Rainer and van der Wall, Berend G. and Schneider, Oliver and Holthusen, Hermann and Postma, Jos (2019) The second Wind-tunnel test of DLR's multiple swashplate system. CEAS Aeronautical Journal, 10 (2), pp. 385-402. Springer. doi: 10.1007/s13272-018-0323-2. ISSN 1869-5590. Volltext nicht online.

Küfmann, Philip and Bartels, Rainer and van der Wall, Berend G. and Schneider, Oliver and Holthusen, Hermann and Postma, Jos (2017) Individual Blade Control of a 5-bladed Rotor Using the Multiple Swashplate System. 6th ARF & Heli Japan 2017, 2017-11-07 - 2017-11-09, Kanazawa, Japan. Volltext nicht online.

Liersch, Carsten M. and Huber, Kerstin Claudie and Schütte, Andreas and Zimper, Dirk and Siggel, Martin (2016) Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configuration. CEAS Aeronautical Journal, 7 (4), pp. 677-694. Springer. doi: 10.1007/s13272-016-0213-4. ISSN 1869-5582.

Loeser, Thomas and Rohlf, Detlef (2014) Experimental Determination of Dynamic Derivatives in a Wind Tunnel Using Parameter Identification. In: 19th STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics, 2014, 10, pp. 651-662. Springer International Publishing. 19. DGLR-Fachsymposium der STAB, 2014-11-04 - 2014-11-05, München. doi: 10.1007/978-3-319-27279-5_57. ISBN 978-331927278-8. ISSN 1612-2909.

Löser, Thomas and Vicroy, Dan D. and Schütte, Andreas (2009) SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Marggraf-Micheel, Claudia and Rütten, Markus and Piewald, Carina (2010) Thermal Comfort in the Aircraft Cabin: The Potential of Objective and Subjective Measurement. In: Proceedings of the CEAS 2009 (Paper ). CEAS 2009, 2009-10-26 - 2009-10-29, Manchester, UK. ISBN 1857682130.

Rossignol, Karl-Stéphane and Pott-Pollenske, Michael and Delfs, Jan Werner and Silberman, Jakob and Gomes, Jorge (2017) Investigating Noise Shielding by Unconventional Aircraft Configurations. 23rd AIAA/CEAS Aeroacoustics Conference, 2017-06-05 - 2017-06-09, Denver. doi: 10.2514/6.2017-3195. 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 Huber, Kerstin Claudie and Boelens, Okko J. and van Rooij, Michel (2016) STATIC AND DYNAMIC NUMERICAL SIMULATIONS OF A GENERIC UCAV CONFIGURATION WITH AND WITHOUT CONTROL DEVICES. NATO STO - Science and Technology Organisation. [Other] Volltext nicht online.

Schütte, Andreas and Huber, Kerstin Claudie and Frink, Neal T. and Boelens, Okko J. (2016) Stability and Control Investigations of Generic 53 Degree Swept Wing with Control Surfaces. Journal of Aircraft, 55 (2), pp. 502-533. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C033700. ISSN 0021-8669. Volltext nicht frei.

Stadler, Hannes and Bauknecht, Andre and Siegrist, Silvan and Flesch, Robert and Wolf, Christian C. and van Hinsberg, Nils and Jacobs, Markus (2017) Background‑oriented schlieren imaging of flow around a circular cylinder at low Mach numbers. Experiments in Fluids, 58 (114), pp. 1-12. Springer Nature. doi: 10.1007/s00348-017-2398-7. ISSN 0723-4864. Volltext nicht frei.

Ströhlein, Tobias and Kleineberg, Markus and Hanke, Michael and Herbeck, Lars (2006) Infusion Technology for Automated Prodcution of High-Performance CFRP-Parts. In: 25TH INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES, p. 330. ICAS 2006, 2006-10-03 - 2006-10-08, Hamburg. ISBN 0-9533991-7-6. Volltext nicht online.

Vicroy, Dan D. and Löser, Thomas and Schütte, Andreas (2009) SACCON UCAV FORCED OSCILLATION TESTS AT DNW-NWB AND NASA LANGLEY 14ft × 22ft TUNNEL. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Zimper, Dirk and Huber, Kerstin Claudie (2018) EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF UNSTEADY AERODYNAMIC DERIVATIVES FOR A GENERIC LAMBDA WING UCAV CONFIGURATION. Deutscher Luft- und Raumfahrtkongress 2018, 2018-09-04 - 2018-09-06, Friedrichshafen. Volltext nicht frei.

Zimper, Dirk and Huber, Kerstin Claudie (2019) Experimental and numerical investigations of unsteady aerodynamic derivatives for a generic lambda wing UCAV configuration. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-019-00426-w. ISSN 1869-5582. Volltext nicht online.

de Groot , Klaus and Egami, Yasuhiro and Klein, Christian and van Schinkel, Ronald and Wubben, Frenk (2009) Titel confidential. Project Report. HST-2008-32. 77 S. Volltext nicht online.

van Hinsberg, Nils and Schewe, Günter and Jacobs, Markus (2017) Experiments on the aerodynamic behaviour of square cylinders with rounded corners at Reynolds numbers up to 12 million. Journal of Fluids and Structures (74C), pp. 214-233. Elsevier. doi: 10.1016/j.jfluidstructs.2017.08.002. ISSN 0889-9746. Volltext nicht online.

van der Wall, Berend G. and Keßler, Christoph and Delrieux, Yves and Beaumier, Philippe and Gervais, Marc and Hirsch, Jean-Francois and Pengel, Kurt and Crozier, Pascal (2017) From ERATO Basic Research to the Blue Edge Rotor Blade. 6th ARF & Heli Japan 2017, 2017-11-07 - 2017-11-09, Kanazawa, Japan. Volltext nicht online.

van der Wall, Berend G. and Keßler, Christoph and Delrieux, Yves and Beaumier, Philippe and Gervais, Marc and Hirsch, Jean-Francois and Pengel, Kurt and Crozier, Pascal (2016) From ERATO Basic Research to the Blue Edge Rotor Blade. AHS International 72nd Annual Forum & Technology Display, 2016-05-17 - 2016-05-19, West Palm Beach, Florida, USA. Volltext nicht online.

van der Wall, Berend G. and Keßler, Christoph and Delrieux, Yves and Beaumier, Philippe and Gervais, Marc and Hirsch, Jean-Francois and Pengel, Kurt and Crozier, Pascal (2017) From Aeroacoustics Basic Research to a Modern Low Noise Rotor Blade. Journal of the American Helicopter Society, 62 (4), pp. 1-16. American Helicopter Society. doi: 10.4050/JAHS.62.042001. ISSN 0002-8711. Volltext nicht online.