United States
•Led structural analysis and certification for satellite programs, driving technical decisions •Developed and implemented advanced finite element models using NASTRAN, Abaqus, and Patran for composite and metallic structures •Supported root cause analysis, test correlation, and design validation to ensure structural integrity and mission success •Conducted load path analysis, structural optimization, and weight reduction initiatives to meet program performance and airworthiness requirements •Collaborated with cross‑functional teams, design engineers, and test teams to resolve complex technical issues and support engineering changes
• Detailed finite element analyses of critical aircraft structural components were performed using NASTRAN, Abaqus, and Patran, covering static strength, fatigue, durability, and damage tolerance assessments •High-fidelity finite element models were developed, validated, and maintained, including mesh optimization, load case definition, boundary condition setting, and material property settings for composite and metallic structures •Load path analyses were performed to verify structural integrity and support design optimization to meet stringent performance, weight efficiency, and airworthiness requirements •Cross-functional collaboration with design engineers, systems engineers, and test teams was undertaken to solve complex technical problems and drive design iterations
•Conducted finite element analysis using NASTRAN, Abaqus, and Patran to perform structural static, fatigue, and durability analysis for aerospace components •Collaborated with design engineers and cross‑functional teams to resolve structural performance issues, optimize component design, and improve product strength and weight efficiency •Performed structural load path analysis and generated technical reports in compliance with Boeing engineering standards and FAA certification requirements