(PhD in Physics, Master d'Ecole Polytechnique, dipl.ing. aerospace)
PROFESSIONAL INTERESTS: Job positions in R&D or research in aerospace field; availability: end of April
2009 – 2013 CNES & CNRS Institute of Combustion Aerothermodynamics Reactivity & Env.
(PhD researcher), , , . , 
► Complete planning and management of the research project in the framework of CNES Perseus program.
► Evaluation of the investigation axes, design of the models; Design & production of elements, installation of wind-tunnel and diagnostic tools. Leading and performing experiments.
► Numerical modelling, grid design, preprocessing CPS_C case, extracting, translating postprocessing analysis.
► Investigation from the fundamental problem to the real in-flight analysis and applicability. Resolving bounded supersonic cross-flows, shock interaction field, pressures, skin friction, all exerted forces and combustion chemical kinetics.
2009 CNRS-ICARE / CNES ( 6 months intern)
► Fluidic thrust vectoring of the conical C-D nozzle
► Experiment installation and setup, bi-color Toepler’ Z-Schlieren installation.
► 3D CFD approach comprising of: meshing, preprocessing, FLUENT numerical simulations, Matlab analysis.
2008 ECOLE POLYTECHNIQUE / ONERA  (3 months student project)
► FSS and RSS (free and restricted shock separation) and cap-shock pattern of the ONERA' TOC launcher nozzle.
► Preprocessing and performing elsA CFD simulations. Postprocessing, RSS stability analysis in Matlab
2006-2007 Aeronautical institute et Mechanical Engineering, Belgrade U. (eng. assistant)
► Complete CATIA design of the plan-tapered wing of UTVA aircraft prototype with mechanization.
► CATIA design and ANSYS DYNA structure analysis of the ultra-light helicopter landing gear.
2013 Doctoral School of Science&Technology of University of Orleans
♦ PhD in Physics, sub. fluid mechanics and energetics, spec. aerothermodynamics.
♦ Defense on 12/04/2013
2009 ECOLE POLYTECHNIQUE
♦ Master of Science in Fluid Mechanics and Energetics
2007 Faculty of Mechanical Engineering, University of Belgrade
♦ dipl. engineer in mechanical & aerospace engineering (5 years degree)
♦ Major: Aeronautical Engineering
♦ diploma dissertation: Fluid-Structure Interactions of the plan-tapered aircraft wing model.
COMPETENCE & LANGUAGES
Aerospace engineering, aerothermodynamics, propulsion, fluid mechanics, stability/control, fluid-structure interactions, physics, plasmas.
CFD: • RANS, uRANS – standard & RNG k-ε, k-ω, k-ω2
• LES, DES – trainee
Codes: elsA, CPS_C, FLUENT, Open FOAM
Analysis: Tecplot, Paraview, Matlab, Scilab
Structural: Modal analysis, deflection, stability. Software: ANSYS, NASTRAN/PATRAN
CAD/CAM: CATIA V5, Solid Works, Autodesk Inventor
Coding: FORTRAN – average | LabVIEW G-coding – high
C, Python – basic level
Languages: English – full professional /scientific (TOEFL 613/640, GRE Math 790/800 in 2005)
Français – intermediate | Russian – advanced | Serbo-Croatian – mother tongue
2012 UN/IAF grant and award at 63rd IAC, Industry group
2012 AIAA Aerodynamics workshop, Atlanta, USA
2010 Plasma physics summer school, Bad Honnef, Germany
2009 EADS, Dassault, Snecma - Aerospace Challenge; Study of the principal propulsion system of the orbital vehicle.
Subject: Secondary injection fluidic thrust vectoring of an axisymmetric supersonic nozzle
Jury: A. Chpoun (dir.), I. Gokalp, K. Kontis, P. Bauer, D. Zeitoun, L. Leger, D. Davidenko, S. Palerm
 V. Zmijanovic, A. Chpoun, B. Rasuo. Flow separation modes and side phenomena in an overexpanded nozzle.FME Transactions, 40(3): 111–118, 2009.
 M. Sellam, A. Chpoun, V. Zmijanovic, and V. Lago. Fluidic thrust vectoring of an axisymmetric nozzle: An analytical model.Int. J. Aerodynamics, (2): 193–209, 2012.
 V. Zmijanovic et al. Thrust vectoring effects of a transverse gas injection into a supersonic cross flow of an axisymmetric convergent divergent nozzle, Progress in Propulsion Physics, vol.4., 227–256, EDP Sciences, 2013.
 V. Zmijanovic et al. Shock vector control of an axisymmetric conical C-D nozzle via secondary transverse gas injection. J. Shock Waves, 23(3), 2013.
 V. Zmijanovic et al., J. Physics of Fluids & J. Propulsion and Power (in preparation)
 AIAA-2012-3874 V.Zmijanovic et al. Experimental and Numerical Study of Transverse Gas Injection into a Propulsive Axisymmetric C-D Nozzle.
 AIAA-2012-5932 V.Zmijanovic et al. Effects of the Inlet Gases Thermodynamic Properties on FTV Supersonic Nozzle.
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