Position: Stress -Analysis and Simulation
Location: Toronto, Canada
Full time role.
Note: We need candidates who have more than 5 + Years of strong experience in aircraft structure.
Job Description:
Execute Stress analysis projects of Aircraft fuselage structures to ensure structural integrity using FEM tools like Nastran, Patran and Hypermesh and classical hand calculation approach using standard aerospace books.
• Structural Analysis:
Perform static, dynamic, and fatigue analysis of aircraft components and assemblies.
• Finite Element Modeling:
Create and refine finite element models (FEMs) for detailed stress analysis.
• Load and Stress Calculations:
Extract loads, stresses, and material data from drawings and specifications.
• Sizing and Design:
Conduct sizing of primary and secondary structural parts to meet static and fatigue requirements.
• Joint Analysis:
Perform detailed analysis of joints and fasteners, including calculating reserve factors for various failure modes.
• Certification and Reporting:
Prepare stress certification dossiers and reports, ensuring compliance with regulatory requirements.
• Problem Solving:
Identify and implement solutions for potential structural issues, such as low reserve factors or buckling.
• Collaboration:
Work with design, loads, and certification teams to ensure a robust and safe design.
• Testing:
Develop and interpret test results to validate analytical models.
• Software Proficiency:
Utilize software like HYPERWORKS, PATRAN, NASTRAN and hands on design softwares like CATIA.
