Engineering Engineer

Profile

Seeking an entry level opportunity to advance my skills while

simultaneously contributing positively to the industry. Specializing in aerospace propulsion, rocket and gas turbine systems in particular. Motivated to transition from a consistent academic to an excellent engineer.

Education

MTech [2018-2020]

Indian Institute of Technology, Kharagpur

Aerospace Engineering / CGPA 9.1

Thesis: Effects of Copper and Silicon Particles on the Combustion Characteristics of Boron-HTPB based Solid Fuels for Hybrid Gas Generator Applications

BTech [2012-2016]

Sri Indu College of Engineering and Technology

Aeronautical Engineering / 85.39%

Project: Experimental Testing Methodology of Liquid Propulsion Thrusters

Intermediate Education [2010-2012]

Little Flower Junior College, Uppal / 87.1%

Areas of Interest & Expertise

Rocket Propulsion

Computational Fluid Dynamics

Gas Turbine Theory

Design of Compressors and Turbines

Advanced Gas Dynamics

Contact

Technical Skills

Software: Ansys, GasTurb

Languages: C, MATLAB, Python, Java

Achievements

Ranked within 98th percentile in the

country in the Graduate Aptitude Test for

Engineers

Jesse Samuel Thomas

MTech in Aerospace Engineering

Projects

Effects of Copper and Silicon Particles on the Combustion Characteristics of Boron-HTPB based Solid Fuels for Hybrid Gas Generator Applications I.I.T. Kharagpur

Under the Guidance of Dr. Srinibas Karmakar

• Investigated the potential of Copper and Silicon particles in improving the poor burning properties of Boron loaded HTPB in gaseous oxygen environment.

• Preliminary analysis was done through NASA CEA software.

• FE-SEM and XRD results were used to determine material properties of Copper and Silicon particles.

• Bomb Calorimeter and Thermo-gravimetric Analysis results were used to investigate the calorific value and kinetics of the fuel.

• Obtained regression rate data using an Opposed Flow Burner setup. Experimental Testing Methodology of Liquid Propulsion Thrusters DRDL Kanchanbagh, Directorate of Liquid Propulsion Under the Guidance of MA Mallesh

• Analysed the experimental methodology used by the Defence Research and Development Laboratory to test liquid propulsion thrusters of various capacities.

• Focused on the experimental method contrasting it with the analytical and numerical method and its implementation using specialized equipment. Gas Turbine Assembly

BHEL Ramachandrapuram

• An analysis of the assembly procedures used by Bharat Heavy Electronics Limited for a gas turbine engine.

Academic Projects

Re-design and Analysis of Components of a Rolls Royce AE3007 Engine

• Worked in a team to re-design the Axial Compressor of the engine. Obtained and compared First Power, Free Vortex and Exponential designs.

• Worked in a team to re-design the Axial Turbine of the engine. Obtained and compared Free Vortex and Constant Nozzle designs.

Steady-State Thermal Analysis of a Rectangular Plate

• Used MATLAB to carry out computations to determine temperature distribution over a flat plate at various mesh sizes.

• Used different schemes such as Jacobi Iterative, Point Gauss Seidal Iterative and Point Successive Over-Relaxation to obtain results and compared them for convergence time.

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