Aerospace Engineering student with background in power generation. Strong technical proficiency with work history in power generation. In-depth knowledge of Autodesk Inventor, Fusion 360, Rhino3D, Rhino CAM, Solid Works, Simulink, and Matlab coupled with maintenance, inspection, airworthiness evaluation, and engineering abilities. Proven history of engineering judgement, decision making, rules compliance enforcement, clear communication and proactive engagement.
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Completed coursework in Aerospace Propulsion, Nuclear-Fossil Fuel-and Sustainable Energy, Thermodynamics, Computational Mechanics, Mechanics of Solids, Mechanics of Aerostructures, Spacecraft Dynamics, Compressible Flow, Systems Analysis and Control, Aerodynamics of Aerospace Vehicles, Aircraft Design I, Aircraft Flight Mechanics, Aerospace Laboratory I, Aerospace Laboratory II, and Spacecraft Design I.
Career Project Highlights
Autodesk Inventor Certified User 2015 to Present Certified by Autodesk as a proficient user of Autodesk Inventor.
Aircraft Design Projects:
Produced a preliminary design of a high-capacity short-range passenger aircraft abiding by 14 CFR Part 21 - 25 and 33 - 34. Responsible for aerodynamics design and performance evaluation of the aircraft. Performed sizing and iterative designs on major aircraft components. And, evaluated the aerodynamic performance of all design iterations of the aircraft as it moved through the iterative design process.
Assessed and evaluated the flight performance of a preliminary aircraft design in a thorough and detailed manner. Built simulation models to test flight performance for key mission requirements of the objective flight envelope, hence; avoided risks and high costs involved in producing and testing a new aircraft through physical testing.
And, evaluated the assessment results of the preliminary design for compliance with mission parameters and FAA regulations for the specified passenger class aircraft.
Aerospace Laboratory Final Project:
Proposed a flight turbulence reduction system for the A-7D Corsair aircraft. Designed a preliminary gust alleviation system based on the pitching moment acting on the main wings. And, configured the system for real-time flight data retrieval, synthesis, and feedback.
Spacecraft Design Final Project:
Developed a preliminary CubeSat design for low earth orbit with the capability of detecting and recording infrasound waves to better understand the nature and future applications of infrasound in detecting seismic activity on earth. Evaluated the preliminary design to meet all system requirements with acceptable risk, cost, and schedule constraints. Determined the mission success criteria, power budget, and number of CubeSats supported. Followed by designing and sizing electrical power and thermal control systems for the SeismicSat.
Power Plant Projects:
Proposed a method to melt iron resourcing concentrated solar power from a solar tower. Designed and sized a preliminary design of a concentrated solar power system capable of generating hot blast air for a blast furnace to melt a few tons of iron or steel.
Proposed utilizing existing nuclear energy infrastructure and concentrated solar power (CSP) technology in conjunction to produce hydrogen via solar and nuclear thermal high temperature electrolysis methods. Surveyed a suitable region for a CSP-Nuclear hydrogen production plant, determined the electrolyzer system suitable for generating hydrogen from high heat steam electrolysis, and designed and sized the CSP system and the accessory steam generator system of the nuclear power plant.
Proposed a ducted fan based vertical takeoff and landing system (VTOL) for jet aircraft to replace the current state-of-the-art VTOL technology used in jet aircraft with a higher energy efficient system. Determined a suitable source in the jet engine to power the ducted fans. Designed and sized the vertical thrust generating ducted fans to completely utilize the power drawn from the jet engine source. Designed and sized the pneumatic power delivery system for the aforementioned ducted fans.
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