High turning compressor tandem cascade for high subsonic flows-part 2: numerical and experimental investigations L Müller, D Kozulovic, D Wulff, S Fischer, U Stark 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5602, 2011 | 61 | 2011 |
Modellierung des Grenzschichtumschlags bei Turbomaschinenströmungen unter Berücksichtigung mehrerer Umschlagsarten D Kožulović DLR, Bibliotheks-und Informationswesen, 2007 | 56 | 2007 |
Modelling of roughness-induced transition using local variables P Dassler, D Kožulović, A Fiala V European Conference on CFD, ECCOMAS CFD 430, 2010 | 55 | 2010 |
Appropriate turbulence modelling for turbomachinery flows using a two-equation turbulence model T Röber, D Kožulović, E Kügeler, D Nürnberger New Results in Numerical and Experimental Fluid Mechanics V: Contributions …, 2006 | 55 | 2006 |
Flow characteristics of axial compressor tandem cascades at large off-design incidence angles T Schneider, D Kožulović Turbo Expo: Power for Land, Sea, and Air 55225, V06AT35A011, 2013 | 52 | 2013 |
Experimental and numerical analysis of hub-corner stall in compressor cascades E Lewin, D Kozˇulovic´, U Stark Turbo Expo: Power for Land, Sea, and Air 44021, 289-299, 2010 | 52 | 2010 |
Modifications of a two-equation turbulence model for turbomachinery fluid flows D Kožuloviş, T Röber, E Kügeler, D Nürnberger Proceedings of the Deutscher Luft-und Raumfahrtkongress, Dresden, Germany 20, 2004 | 52 | 2004 |
Aerodynamic installation effects of an over-the-wing propeller on a high-lift configuration L Müller, W Heinze, D Kožulović, M Hepperle, R Radespiel Journal of Aircraft 51 (1), 249-258, 2014 | 51 | 2014 |
Modelling the streamline curvature effects in turbomachinery flows D Kozˇulovic´, T Ro¨ ber Turbo Expo: Power for Land, Sea, and Air 4241, 1239-1248, 2006 | 42 | 2006 |
An approach for modelling the roughness-induced boundary layer transition using transport equations P Dassler, D Kozulovic, A Fiala Europ. Congress on Comp. Methods in Appl. Sciences and Engineering, ECCOMAS, 2012 | 37 | 2012 |
The effects of turbulence length scale on turbulence and transition prediction in turbomachinery flows C Bode, T Aufderheide, D Kožulović, J Friedrichs Turbo Expo: Power for Land, Sea, and Air 45615, V02BT39A042, 2014 | 32 | 2014 |
Numerical and Experimental Investigations of a Compressor Cascade Flow With Secondary Air Removal S Pönick, D Kozulovic, R Radespiel, B Becker, V Gümmer ASME Turbo Expo, Vancouver, Canada, GT2011-45202, 2011 | 32 | 2011 |
Comparison of phase-change-heat-pump cooling and liquid cooling for PEM fuel cells for MW-level aviation propulsion TL Kösters, X Liu, D Kožulović, S Wang, J Friedrichs, X Gao International Journal of Hydrogen Energy 47 (68), 29399-29412, 2022 | 27 | 2022 |
Investigations on aerodynamic loading limits of subsonic compressor tandem cascades: end wall flow C Hertel, C Bode, D Kožulović, T Schneider Turbo Expo: Power for Land, Sea, and Air 45608, V02AT37A049, 2014 | 26 | 2014 |
Potential of future thermoelectric energy recuperation for aviation C Bode, J Friedrichs, R Somdalen, J Köhler, KD Büchter, C Falter, U Kling, ... Journal of Engineering for Gas Turbines and Power 139 (10), 101201, 2017 | 24 | 2017 |
An approach for inclusion of a nonlocal transition model in a parallel unstructured computational fluid dynamics code D Kožulović, BL Lapworth | 18 | 2009 |
Unsteady flow simulations of an over-the-wing propeller configuration L Müller, D Kozulovic, J Friedrichs 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3886, 2014 | 16 | 2014 |
Investigations on aerodynamic loading limits of subsonic compressor tandem cascades: Midspan flow C Hertel, C Bode, D Kožulović, T Schneider ASME International Mechanical Engineering Congress and Exposition 56178 …, 2013 | 16 | 2013 |
Outlet Guide Vane Airfoil for Low Pressure Turbine Configurations H Koch, D Kozulovic, M Hoeger 42nd AIAA Fluid Dynamics Conference and Exhibit, 2979, 2012 | 14 | 2012 |
Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number L Müller, D Kožulović, R Radespiel CEAS Aeronautical Journal 5, 305-317, 2014 | 13 | 2014 |