Aerodynamcis, CFD, Computational Heat and Mass transfer, OpenFOAM

Puneet Pushkar

Contact

Information

H.No. ***, Vikash Nagar, Mob: +91-988*******, 775-***-****

Pt.Deen Dayal Upadhaya Nagar, E-mail: ***********@*******.*** Chandauli, Uttar Pradesh (India) LinkedIn ID: pushkar-puneet Education Indian Institute of Science, Bengaluru, Karnataka, India Master of Technology in Aerospace Engineering July 2021 Grade Point Average: 7.6/10

Thesis advisor: Prof S.V. Raghurama Rao

Topic: \Higher order WENO central schemes for hyperbolic conservation laws." A numerical comparative study of higher order Weighted Essentially Non-oscillatory (WENO) schemes for two di erent ux splitting approaches, namely, Local Lax Friedrichs and Rie- mann Invariant-based Contact-discontinuity Capturing Algorithm (RICCA) in nite vol- ume framework was done on various standard shock tube problems. Performance analysis of WENO 3

rd

and 5

th

order schemes was also done.

Feroze Gandhi Institute of Engineering and Technology, Raebareli, Uttar Pradesh, India Bachelor of Technology in Aeronautical Engineering July, 2018 Percentage: 72:94 %

Project advisor: Prof R. K. Singh

Topic: \Tandem rotor, design and fabrication"

Fabricated a tandem rotor UAV modelled on the US Chinook 47 carrier vehicle, incor- porated a 6-DOF ight controller and performed ight parameter calibration on i-Nav Con gurator.

S. G. Public School, Pandit Deen Dayal Upadhyay Nagar, Uttar Pradesh, India Class XII (Science), Central Board of Secondary Education July, 2013 Percentage: 71.4%

Projects Incompressible micro-channel ow analysis and simulation Supervisor: Prof Raghurama Govardhan (IISc, Bangalore) May - June 2021 Solved ow eld in a 2D micro-channel numerically using MATLAB’s inbuilt PDE tool and obtained Reynolds number, friction factor and velocity pro les for rectangular, prismatic and circular channels which were validated against benchmark results. E ect of roughness on channel was also studied with no-slip and perfect slip boundary conditions. Implicit 2D Finite Volume

Prof N Balakrishnan (IISc, Bangalore) October - December 2020 A 2D Convection-Di usion channel ow problem is studied and simulated on a unstructured triangulated mesh on a implicit face based nite volume method. Design analysis of N+1 and N+3 turbofan engines

Prof Pratikash Panda (IISc, Bangalore) October { December 2019 Developed a complete conceptual thermodynamic cycle design framework for N+3 turbofan en- gines in MATLAB; the obtained thermodynamic parameters were compared against available N+1 turbofan engine data. Optimisation of thrust speci c fuel consumption (TSFC) with tur- bine inlet temperature was done at sea level take-o, idle and cruise ight conditions. 1

Achievements Best xed wing RC Model design at Aerotrix modelling and Fabrication workshop, 2015 All India Talent Search Examination (AITSE) Scholarship Award, 2007 Courses Academic coursework: Finite Volume Method, Aerodynamics, Computational Gas Dynamics, Propulsion, Solid and uid phenomena at small scales, Numerical uid ow, Flight mechanics, Numerical linear algebra, Turbo machines in renewable energy.

Independent coursework: Introduction to OpenFOAM, OpenFOAM-Intermediate. Technical Skills Simulation and visualization softwares : OpenFOAM, ParaView

Programming and scripting languages : C++, Fortran, Python, MATLAB

Operating systems : Ubuntu, Windows

Professional

Memberships

Society of Industrial and Applied Mathematics (SIAM) (2019 - present) References Prof S. V. Raghurama Rao Dr Ramesh Kolluru Associate Professor Post-Doctoral Fellow

Aerospace Engineering Department Aerospace Engineering Department Indian Institute of Science Indian Institute of Science Bengaluru, Karnataka (India) Bengaluru, Karnataka (India) E-mail: *****@****.**.** E-mail: ********@****.**.** Prof R. K. Singh

Assistant Professor

Aeronautical Engineering Department

F. G. I. E. T.

Raebareli, U. P. (India)

E-mail: **************@*****.***

2

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