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.