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Senior Stress Engineer - Aerostructures

Senior Stress Engineer - Aerostructures

Infosys Limited
Fresher
Not Disclosed
Early Applicant
  • Posted a day ago
  • Be among the first 10 applicants

Job Description

Job Description:

  • We are seeking an experienced Stress Engineer to perform static fatigue and damage tolerance analysis for aircraft structures
  • This role requires strong expertise in aerospace stress methodologies Boeing standards and advanced analysis tools

Key Responsibilities:

  • Perform static fatigue and damage tolerance analysis using classical hand calculations
  • Apply Boeing Static and Book 1 2 and 3 Fatigue Analysis methodologies
  • Use Boeing stress tools IAS XSA SA FEADMS IDTAS Moss Duberg FAMOSS
  • Extract loads from Finite Element Models and determine critical failure modes
  • Analyze primary and secondary metallic and composite structures
  • Interpret engineering drawings and coordinate with cross functional teams
  • Prepare Engineering Stress Reports ensuring compliance and safety
  • Collaborate with onsite coordinators to meet customer expectations

Technical Requirements:

  • Bachelor s degree in Mechanical or Aerospace Engineering
  • 2 5 years of experience in aerospace stress analysis
  • Expertise in static fatigue and damage tolerance calculations
  • Familiarity with Boeing stress methodologies and tools

Additional Responsibilities:

  • Experience in metallic and composite structural analysis
  • Proficiency in Finite Element Analysis tools Nastran Patran
  • Knowledge of MRB and SRM processes
  • Experience with CATIA V5 Enovia
  • Strong communication and technical report writing skills

Preferred Skills:

Domain->Aerospace->Aerospace Basics,Technology->CAD->CATIA->CATIA V5,Technology->Finite Element Analysis->Finite Element Analysis - Others

More Info

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Key Skills

Boeing stress tools IAS

Duberg

XSA

metallic and composite structural analysis

MRB and SRM processes

FEADMS

FAMOSS

Boeing Static and Book 1 2 and 3 Fatigue Analysis methodologies

IDTAS

static fatigue and damage tolerance calculations

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