As a driven and determined second-year Aeronautical Engineering student at De Montfort University, Leicester, I've gained a strong grounding in aerospace principles and technologies over my first year of study. Academic life has been marked by an ever-present striving not only for comprehension of the theoretical but also for application of such to real engineering issues. I possess a sharp analytical mindset, developed through rigorous studies and project work, which enables me to solve problems effectively and contribute positively to technical projects. An aspiration to create and contribute to the development of the aerospace industry fuels my passion for aerospace. I am actively seeking challenges to gain greater insight through real experience, experience sharing with competent professionals, and solving complex engineering problems. I am eager to use my growing expertise and enthusiasm within an active aerospace environment, where I can maximize my skills and contribute positively.
Applied flight mechanics principles to design and analyze Boeing 737-800 performance parameters like thrust, altitude, airspeed, range, and climb rate, and from mathematical modeling determined lift, drag, and stability, developing technical analysis skills, simulation capabilities, and in-depth knowledge about aircraft design, operation, and aviation safety.
Modeled and analyzed aircraft performance by estimating weight distribution and center of gravity (CG) for stability, calculating the Mean Aerodynamic Chord (MAC) to analyze aerodynamic characteristics, analyzing moment of inertia for rotational dynamics, and analyzing airfoil lift and drag characteristics using XFLR5 software, resulting in proficiency in aircraft mass and aerodynamic analysis, technical report writing skill enhancement, and XFLR5 simulation skill.
Modelled an aircraft in XFLR5 from technical schematics to produce a scaled 3D model with detailed wing, fuselage, and control surface features, followed by mass/inertia calculation and aerodynamic/stability test, leading to aircraft design analysis, 3D modeling, and aerodynamic performance assessment skills.
Utilized Creo Parametric to create detailed 3D models of assemblies and components focusing on structural optimization and mass minimization using forces applied analysis with strict adherence to exact engineering requirements and developing competencies in force simulation, structural analysis, and mass optimization techniques.
Analyzed Nissan Leaf performance data using MATLAB to assess efficiency and power consumption, importing and processing data to extract key metrics like speed, SOC, and battery data, creating visualizations, and analyzing power distribution, resulting in expertise in MATLAB data analysis and electric vehicle performance evaluation.