Stress Analysis Engineer

Tata Technologies Europe; Bristol; On-site; GBP 80,000 - 100,000; Full time

Job summary

A leading technology company in the UK is seeking Stress Analysis Engineers at Mid, Senior, and Lead levels to manage the static analysis of fuselage and wing structures for utility aircraft. The ideal candidate will have deep expertise in metallic and composite stress analysis, DFEM/GFEM modelling, and certification compliance. The role includes responsibilities for planning, reviewing, and approving deliverables, as well as mentoring junior engineers. This position offers the opportunity to work on exciting aerospace projects within a collaborative environment.

Qualifications

• Experience leading and managing static analysis for fuselage and wing structures.
• Ability to ensure analytical rigor and support certification activities.
• Skill in mentoring junior stress engineers.

Responsibilities

• Lead static stress analysis for fuselage and wing structures under multiple load conditions.

Skills

Deep expertise in metallic and composite stress analysis

DFEM / GFEM modelling

Certification compliance

Weight optimization

Job description

At Tata Technologies we make product development dreams a reality by designing, engineering and validating the products of tomorrow for the worlds leading manufacturers.

We are growing our capability within Aerospace division specifically, Stress Analysis Engineers at Mid, Senior and Lead level. This is due to an increasing pipeline of projects with our Aerospace clients.

Role Overview :

We are looking for a Stress Analysis Engineers to lead and manage the static analysis of fuselage and wing structures for utility aircraft. The role requires deep expertise in metallic and composite stress analysis, DFEM / GFEM modelling, certification compliance, and weight optimization.

You will be responsible for planning, reviewing, and approving analysis deliverables, ensuring analytical rigor, and supporting certification activities while mentoring junior stress engineers and driving collaboration across design, loads, and manufacturing functions.

Responsibilities :

• Lead static stress analysis for fuselage and wing structures under multiple load conditions.