Own GFEM updates, FEM validation, and DMU optimization.Define mesh strategies for complex stress/F&DT analyses.
Lead load extraction, hand calcs, and crack growth assessments.
Conduct fatigue life predictions (rainflow/Miner) and damage tolerance evaluations.
Validate composite/metallic material performance in ISAMI.
Manage complex static and fatigue analysis, including crack growth and DTA for metallic and composite structures.
Ensure compliance with Airbus structural analysis methods and tools.
Develop Excel VBA tools for process automation.
Drive and ensure Airframe certification requirements and resolve critical structural issues.
Guide junior engineers and review analysis reports.
Review technical reports, Liaise with Technical committee for design verification and changes.
conduct technical audits, and support management decisions.
Qualifications:
Master's in Aerospace/Mechanical Engineering (PhD a plus).
9+ years in airframe stress/F&DT (fuselage sub-assemblies: frames, panels, junctions).
Expert in Airbus methods, ISAMI, HyperWorks, Nastran/Patran.
Deep knowledge of composite/metallic fatigue and crack growth.
Advanced Excel/VBA/Python for analytical automation.
Good Communication skills
Now
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Job Detail
Job Id
JD3797130
Industry
Not mentioned
Total Positions
1
Job Type:
Full Time
Salary:
Not mentioned
Employment Status
Permanent
Job Location
KA, IN, India
Education
Not mentioned
Experience
Year
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MNCJobsIndia.com will not be responsible for any payment made to a third-party. All Terms of Use are applicable.