• Perform Finite Element modeling and analysis on aircraft structures, ensuring structural integrity and safety. • Conduct rigorous Finite Element Analysis (FEA) to validate designs and assess structural performance. • Utilize rigid body hand calculations to complement FEA results and ensure accurate analysis. • Create comprehensive interface load (IFL) reports for precise assessment of structural components for customers. • Conduct weight and balance analysis to optimize aircraft performance and stability. • Developed a streamlined method using VBA for rigid body hand calculations, reducing total time by 2/3rd compared to previous approaches. • Apply strong knowledge of structural mechanics and stress analysis principles to ensure compliance with industry standards. • Meticulously ensure the structural integrity of aircraft components and systems. • Collaborate with multidisciplinary teams to support design optimization and problem-solving initiatives. • Demonstrate meticulous attention to detail and a strong commitment to quality and accuracy in all analysis tasks.

• Conducted structural analysis of piece parts for 3D models of space antennas using FEMAP, NASTRAN, and MathCAD for accurate performance assessment.• Served as a Test & Integration Engineer, providing on-floor support for the proper stowage and deployment of space antennas and conducting tests on critical piece parts to ensure optimal functionality.• Worked as a Design Engineer, responsible for 3D modeling of space antenna piece parts, assembly tooling, and designing sub-assemblies using PTC Creo software.• Created detailed 2D drawings in compliance with ASME Y14.5 and GD&T standards, facilitating precise manufacturing and assembly processes.• Facilitated table top reviews and incorporated redlines to improve design accuracy and effectiveness.• Assisted in the development of Interface Control Designs (ICDs) and Engineering Change Orders (ECOs) to maintain project specifications and documentation integrity.• Managed the release of parts in the Product Data Management (PDM) system for effective product life cycle management and coordination with manufacturing teams. • Calculated critical clearances of different piece parts in top-level assemblies to ensure proper fit and functionality.• Tracked drawing release curves for programs and provided weekly updates to the team.• Contributed to the enhancement of the Engineering manual, serving as a comprehensive guide for design and drawing best practices across the Mechanical Engineering department, resulting in improved consistency, accuracy, and cost savings for the company.

US Army Reserve

Project: Systems for Prosthetic Alignment Utilizing Real-Time Kinematics (SPAURK)

Roles and Responsibilities:1. To fabricate graphene/nanoclay reinforced epoxy composite and perform Dynamic Mechanical Analysis (DMA), Thermo Mechanical Analysis (TMA, and Flexure test on the samples to characterize its mechanical thermal properties.2. To fabricate hybrid carbon fiber/glass fiber reinforced epoxy composites for marine application and perform Low Velocity Impact (LVI) Test

Project Title: Simulation of Bio-Inspired Porous Battery Electrodes for nanoHUB.org

Tutor for Physics, Pre-Calculus and General chemistry

Calibration of Pyramidal Balance for Wind TunnelParticle Image Velocimetry ProjectDesign Build Fly project (Structure & Safety team)

Self Healing of E-glass/Epoxy composite using hollow glass fibres Self Healing of E-glass/Epoxy composite using microcapsulesAnnual report preparation

Flight Simulationa and UAV projectZero-Gravity Experiment Project

Flight simulation and lab works

Managed the office of professor and helped in citation

Volunteered for Open House 2012Mentor for Freshman students of Fall 2013