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Dragan Kozulovic
Dragan Kozulovic
Universität der Bundeswehr München, Institute of Jet Propulsion
Bestätigte E-Mail-Adresse bei unibw.de - Startseite
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Zitiert von
Zitiert von
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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
582011
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
552006
Modellierung des Grenzschichtumschlags bei Turbomaschinenströmungen unter Berücksichtigung mehrerer Umschlagsarten
D Kožulović
DLR, Bibliotheks-und Informationswesen, 2007
532007
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
522004
Modelling of roughness-induced transition using local variables
P Dassler, D Kožulović, A Fiala
V European Conference on CFD, ECCOMAS CFD 430, 2010
512010
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
502010
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
462014
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
452013
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
402006
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
332012
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
282011
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
262014
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
242017
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
232014
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
192022
An approach for inclusion of a nonlocal transition model in a parallel unstructured computational fluid dynamics code
D Kožulović, BL Lapworth
182009
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
152014
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
142013
Outlet Guide Vane Airfoil for Low Pressure Turbine Configurations
H Koch, D Kozulovic, M Hoeger
42nd AIAA Fluid Dynamics Conference and Exhibit, 2979, 2012
142012
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
122014
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