Dedicated and passionate Aerospace Engineer with a strong foundation in design and quality. Committed to leveraging my expertise to drive the success and advancement of organizations within the aerospace industry. Focused on contributing to the growth and reputation of the organization by applying innovative solutions and strategic insights to propel it as a leader in the aerospace sector.
·As a Quality Control Associate for Civic and CR-V cars, my primary responsibility involved conducting comprehensive quality checks on engine components, particularly cylinder heads and blocks. Adhering strictly to industry standards and internal quality protocols, I ensured that each component met the highest performance and quality benchmarks. Throughout my tenure, I consistently upheld the reputation of our company by delivering top-tier results and demonstrating a collaborative approach to problem-solving within the team.
My area of expertise is carrying out complex evaluations with an emphasis on the Su-30 MKI aircraft's aerodynamic properties. I carefully research and examine the intricate airflow dynamics related to the delta wing design using cutting-edge computational fluid dynamics (CFD++) software in an effort to improve the Su-30 MKI's aerodynamic performance and manoeuvrability.
We received a prototype for analysis along with an installation and setup manual. Our daily tasks involved testing the prototype and analyzing the results with the team. We utilized ANSYS for the analysis of both prototypes and real-life models. Following numerous tests, we engaged in team discussions to determine the optimal geometrical conditions.
Mechanical design Software: Catia V5
Other Software: MATLAB and MS Office
Process Improvement tools: Statistical process control and 7QC tools
Soft skills: Critical thinker, adaptive, creative, and effective communicator
· In this project, the validation of Non-slender Delta wing simulation data which is performed on CFD++ software with experimental results. Based on the various literature survey, importance of delta wing and its data for validation were identified. The CATIA V5, SpaceClaim 22R1, EXCEL and CFD++ were used for the 3D modelling, geometry clean-up, meshing, pre and post-processing. In this project the main focus on the validation of simulation data with experimental results. The 3D modelling is done in CATIA V5, where clean-up is done by the help of SpaceClaim 16.2. The simulation is carried out by CFD++.
· Researched Indian Space Research Organization's Mars Orbiter Mission (MOM), analyzing launch trajectory, Hohmann transfer, and aerobraking. Evaluated key parameters including AOP, RAAN, and aerodynamic techniques for optimizing interplanetary trajectory.
· The objective of this project is to develop a comprehensive simulation model of an omnidirectional robot using MATLAB and Simulink. The project will encompass various aspects including kinematics, dynamics, control algorithms, and trajectory planning. Through this simulation, we aim to explore the intricate mechanics and behaviors of omnidirectional robots, understand their motion characteristics, and design efficient control strategies for optimal performance .