Stress Engineer/Structural Analysis Engineer
Politecnico di Bari – sede di TARANTO, Q.re Paolo VI –
€ competitive
start: July 2022,
Primary Location: : TARANTO, Politecnico di Bari
Job Type: office and smart working
CV to talentsforsator@satorsrl.it (rif. Code SE_InN_2022)
A Stress Engineer will be working as a member of a SATOR engineering team to make stress & thermal analysis on aerospace component. For this reason an interest in defence engineering and development is key to this opportunity.
Responsibilities include:
- Identify strength and stiffness requirements and perform structural analysis (static, demage tolerance) to ensure requirements are met with a minimum mass design.
- Provide a detailed definition of all structural testing required to verify that strength and stiffness requirements are met.
- Monitor tests and write test assessment reports.
- Ensure that the design incorporates all features necessary to meet the strength and stiffness requirements.
- To be conversant with and to apply as appropriate, analysis techniques and methods for light weight structures strength and stiffness prediction that are generally common to aircraft structures analysis. These will include classical hand analysis and computer techniques including the use of the industry standard NASTRAN finite element programme with Patran/HyperMesh/HyperView and other pre and post processing software.
- Write clear and concise strength summary reports (English language) demonstrating adequate strength margins for all significant possible modes of failure. Write other associated analysis documentation.
To present strength and stiffness analyses and test requirements and assessments at formal design reviews.
· Provide design support to manufacture to ensure that strength and stiffness requirements are met for all non-conformances to design with appropriate corrective action.
Qualifications, Skills & Experience
Essential:
- Degree qualified or equivalent in Mechanical or Aeronautical Engineering or similar discipline
- Demonstrable experience in performing detailed stress analysis (hand calcs) and FE modelling (NASTRAN/Patran, HyperMesh, HyperView) for lightweight metallic structures in the aerospace industry