CFD Engineer

Petr Kazarin

+1-386-***-**** ************@*****.***

Summary

• Participation in team competition: designed the aerodynamics package for Formula SAE car (CAD/CFD)

• Proficient in computation modeling and analyses of fluid dynamics with commercial software: OpenFOAM/ANSYS Fluent, parallel computing, visualization, and post- processing (Paraview/Tecplot)

• Advanced skills in geometry meshing (SnappyHexMesh/CfMesh/Pointwise)

• More than 4 years of code development experience (C++/Matlab) and bash shell scripting

• 3 years of work as a TA and instructor in the wind tunnel lab: setting up and conducting experiments in the wind tunnel

• Broad experience in fluid mechanics theory, modeling and applications Qualifications

CFD software: OpenFOAM, Ansys Fluent, Tecplot, Paraview CAD: CATIA

Grid generation: SnappyHexMesh, CfMesh, Pointwise

Programming languages: C/C++, Matlab, Fortran, bash Computer skills: Linux, Windows

Other software: Matlab/Simulink, Netbeans, Microsoft Visual Studio, LATEX, Microsoft Office software

Education

2015-current PhD in Aerospace Engineering

Embry-Riddle Aeronautical University (ERAU), Day-

tona Beach campus, FL

GPA: 4.0/4.0

2012 - 2014 Master of Science in Applied Physics and Mathematics, Moscow Institute of Physics and Technology(MIPT),

Russia, Department of Aeromechanics and Flight Engineering GPA: 3.92/4.0

2008 - 2012 Bachelor of Science in Applied Physics and Mathematics, Moscow Institute of Physics and Technology(MIPT),

Russia, Department of Aeromechanics and Flight Engineering GPA: 3.65/4.0

Professional Experience

PhD student and head TA and RA at ERAU, Daytona Beach, FL, AE Department

(2015 - Current)

• Design and 3D aerodynamic analysis of a Formula SAE car (sufficiently increased the down force as well as the aerodynamic efficiency). Currently working on fur- ther improvement of aerodynamic efficiency by adjusting the existing elements and incorprating new components in the aerodynamic package

• CFD analysis of the Short Take-Off and Landing (STOL) Aircraft (CFD, aerody- namic design)

• Investigation of the formation and evolution of the wingtip vortex (CFD and vali- dation with the experimental data)

• Development of the low-fidelity mathematical model for prediction of the evolution and propagation of the wake vortex (The model is currently being tested by FAA)

• Developed and employed robust nonlinear controller for UAV

• TA and instructor in the wind tunnel lab

Engineer at Aviaavtomatica, Zhukovskiy, Russia (2014)

• Employed the control system for dirigible

• Designed landing gear model for dirigible

Engineer at CIAM, Moscow, Russia (2011 - 2014)

• Developed C++ code for the flow simulation in the cyclic Rotating Detonation En- gine (RDE) combustion chamber and studied its working regimes within jet engine Publications

1. Kazarin, P., The simulation of propagation of the detonation wave in the ring chan- nel, 55-th MIPT Scientific Conference, Moscow-Dolgoprudny-Zhukovsky, Russia 2. Babushenko D.I., Kazarin P.S., K. V. T. N. S. A., Numerical Analysis of Character- istics of Hydrogen-Fueled Model Combustor with Rotating Detonation Wave, 6th International Symposium on Non-equilibrium Processes, Plasma, Combustion, and Atmospheric Phenomena (NEPCAP 2014)

3. Kazarin, P., Provalov, A., Golubev, V., Borener, S., Hafty, D., Crook, I., and Suchkov, A., Terminal-zone wake vortex safety assessment in the context of UAS integration in the NAS, Transportation Research Procedia, Vol. 14, 2016, pp. 1364– 1373

4. Golubev, V., Kazarin, P., MacKunis, W., Borener, S., Hufty, D., and Suchkov, A., Analysis of safety implications for SJA-based robust UAS flight control technology, 2015 IEEE/AIAA 34th Digital Avionics Systems Conference (DASC), IEEE, 2015, pp. 5D1–1

5. Golubev, V. V., Kazarin, P., MacKunis, W., Borener, S., and Hufty, D., Robust SJA-Based Nonlinear Trajectory Tracking Control Using Unmanned Aircraft LPV Model, 2016

6. Kazarina, M., Kazarin, P., Nguyen, L., Golubev, V. V., Borener, S., Hufty, D., Pasiliao, C. L., and Visbal, M. R., Effects of Time-Harmonic Gust and Turbulence on Unsteady Aerodynamic Responses of Loaded Low-Speed Airfoils, 7. Kazarin, P. S. and Golubev, V. V., On Effects of Ground Surface Conditions On Aircraft Wake Vortex Evolution, 9th AIAA Atmospheric and Space Environments Conference, 2017, p. 4368

8. Kazarin, P. S., MacKunis, W., Moreno, C., and Golubev, V. V., Robust Nonlin- ear Tracking Control for Unmanned Aircraft with Synthetic Jet Actuators, AIAA Atmospheric Flight Mechanics Conference, 2017, p. 3730 9. Kazarin, P. S. and Golubev, V. V., Comparison of Probabilistic Approaches for Predicting the Cone of Uncertainty in Aircraft Wake Vortex Evolution, 9th AIAA Atmospheric and Space Environments Conference, 2017, p. 4369 10. Kazarin, P., Kazarina, M., and Golubev, V. V., High-Fidelity Simulations of Terminal- Zone Heterogeneous Terrain Effects On Aircraft Wake Vortex Evolution, 2018 AIAA Aerospace Sciences Meeting, 2018, p. 1279

11. Karpuk, S., Kazarin, P., Gudmundsson, S., and Golubev, V. V., Preliminary Feasi- bility Study of a Multi-Purpose Aircraft Concept with a Leading-Edge Embedded Cross-Flow Fan, 2018 AIAA Aerospace Sciences Meeting, 2018, p. 1744

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