Job Description
Candidate should have 6 to 10 years of positive working experience on stress analysis of Aircraft structural (Primary and Secondary) components. • Candidate should have positive knowledge in Aerospace domain. Candidate should be able to co-ordinate with concerned stakeholders’ teams. Profound knowledge on Stress analysis, aircraft loads and aircraft structures are expected.
Job requirements
Experience with Boeing component design ( Fuselage structure , Systems, Pylons, Nacelles)
Valuable hands-on experience with any FE tools like Patran/Hypermesh
Profound knowledge on Stress analysis, aircraft loads and aircraft structures are expected.
Excellent knowledge on MS tools is mandatory.
Boeing standards experience is preferred
Experience in the preparation of stress reports.
Boeing Inhouse tools. MSC Nastran Patran is an additional advantage, Basic knowledge on Catia V5.
📌 Stress Analysis Engineer Bengaluru (India)
🏢 Infosys
📍 India
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