Vladimir Jovanovic
Senior Research Engineer at Cenaero- Claim this Profile
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Serbian Native or bilingual proficiency
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English Full professional proficiency
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Russian Limited working proficiency
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Dutch Elementary proficiency
Topline Score
Bio
Credentials
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Sports and Building Aerodynamics
Coursera Course CertificatesJan, 2016- Nov, 2024
Experience
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Cenaero
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Belgium
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Research
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1 - 100 Employee
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Senior Research Engineer
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Oct 2022 - Present
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InsPyro
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Belgium
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Operations Consulting
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1 - 100 Employee
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CFD Engineer
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Mar 2018 - Sep 2022
Optimization of processes in metallurgical, chemical, food and industries alike depend on the knowledge of how fluid flow and turbulence affect heat and mass transfer and rate of chemical reactions. These phenomena is very difficult to measure due to opaqueness of the system which is normally at a high temperature. Therefore, modelling of the processes with CFD seems to be the only solution to get some insight into what is happening within. Optimization of processes in metallurgical, chemical, food and industries alike depend on the knowledge of how fluid flow and turbulence affect heat and mass transfer and rate of chemical reactions. These phenomena is very difficult to measure due to opaqueness of the system which is normally at a high temperature. Therefore, modelling of the processes with CFD seems to be the only solution to get some insight into what is happening within.
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CFD Engineer
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Mar 2013 - Feb 2018
We perform mid to large scale CFD simulations on complex geometries for a variety of industrial partners, mainly focusing on indoor ventilation, thermo-fluids systems, power generation, etc. By combining substantial experience in turbulent fluid flow modelling and expertise in some of the most powerful tools in the field such as SpaceClaim for geometry preparation, TGrid and Pointwise for grid generation, and Fluent or OpenFOAM for CFD computation, we are able to deliver reliable results in always limited time frame.
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KU Leuven
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Belgium
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Research Services
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700 & Above Employee
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Researcher Engineer in Computational Aeroacoustics
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2008 - Mar 2013
Implemented and used proper orthogonal decomposition for coherent structure identification in a compressible turbulent flow over an open three dimensional cavity. Large scale Direct Numerical Simulation were employed to generate data for modal decomposition. In addition, the Ffowcs-Williams and Hawkings integral equation was implemented to propagate noise sources to the acoustic far field. Implemented and used proper orthogonal decomposition for coherent structure identification in a compressible turbulent flow over an open three dimensional cavity. Large scale Direct Numerical Simulation were employed to generate data for modal decomposition. In addition, the Ffowcs-Williams and Hawkings integral equation was implemented to propagate noise sources to the acoustic far field.
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Royal Military College of Canada/Collège militaire royal du Canada
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Canada
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Defense and Space Manufacturing
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300 - 400 Employee
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Lecturer in Aircraft Performances and Aircraft Structures
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Sep 2007 - Mar 2008
Teaching courses in Aircraft Performances and Aircraft Structures to the third year students.
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Research Engineer in Experimental Aerodynamics
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Mar 2006 - Mar 2008
Low speed wind tunnel experiments on a symmetric wing which undergoes self-sustained oscillations due to flow instabilities.
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Queen's University
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Canada
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Higher Education
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700 & Above Employee
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Faculty of Mechanical and Materials Engineering
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Sep 2003 - Mar 2006
Developed experimental methodology based on usage of infrared camera and optical filters to pick up in-flight temperature of plastic powder during thermal spray coating process. Developed experimental methodology based on usage of infrared camera and optical filters to pick up in-flight temperature of plastic powder during thermal spray coating process.
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Rocket Propulsion Engineer - Solid Propellant Grain Propulsion Group
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Jan 2001 - Aug 2003
Development and experimental testing of various types of rocket engines mainly used for anti-hail defense.Prediction of aerodynamic coefficients for the supersonic flow around fins. Development and experimental testing of various types of rocket engines mainly used for anti-hail defense.Prediction of aerodynamic coefficients for the supersonic flow around fins.
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Education
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Katholieke Universiteit Leuven
PhD, Aeroacoustics -
Queen's University
MScEng, Mechanical Engineering -
University of Belgrade
Dipl.Ing. (5 years curriculum), Mechanical (Aeronautical) Engineering