10 - 20 years

30 - 40 Lacs

Posted:-1 days ago| Platform: Naukri logo

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Job Type

Full Time

Job Description

Role & responsibilities

  • Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as a coordinated team
  • Structural analysis includes calculation of loads, Static analysis, Fatigue analysis, Damage-Tolerance analysis, and Vibration analysis
  • Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method
  • Generate documentation to report analysis and, test results to support certification/qualification
  • Support Gated Reviews to validate the quality and completeness of work packages
  • Familiar with regulatory framework (FAA and Mil-Spec), for warranting safety and regulatory compliance
  • Bachelors or Masters degree in Mechanical/Aerospace/Applied Mechanics/Structural engineering and should of experience in stress analysis.
  • Must have experience working with multi-functional teams spread across multiple products and locations within Boeing and external partners.
  • Must be flexible, with a high tolerance for organizational complexity and ability to work with partners from within Boeing and outside, across different cultures and time-zones.
  • Communication strong written and verbal communication skills, ability to prepare comprehensive reports, proposals. Candidate must be proficient in English, and familiar with MS Office tools.
  • Candidate must be a self-starter with a positive attitude, high ethics, and a track record of working optimally under pressure in a time-constrained environment.
  • Candidate must demonstrate excellent analytical and problem-solving skills

Preferred candidate profile

  • Experience in structural analysis of various airframe structures.
  • Experience with structural analysis of metallic and composite structures.
  • Experience with static and fatigue analysis
  • Knowledge of airplane operating environments
  • Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, structural loads and analysis methods
  • Experience in applying FEM software (e.g., ABAQUS, LS-DYNA, PATRAN/NASTRAN, Hyperworks)
  • Experience or training with computer programming languages (e.g., Matlab, Python, Visual Basic)
  • Experience in applying industry CAD systems (e.g., NX/Teamcenter and CATIA/ENOVIA)
  • Candidate demonstrates excellent analytical and problem-solving skills
  • Good verbal and written communication skills to liaise with several Collaborators
  • Ability to work across functional teams and organizations
  • Willingness to expand into technical areas without prior experience
  • Desire to continuously improve our airplanes

Typical Education & Experience:

  • Bachelors in Mechanical/Aerospace/Applied Mechanics/Structural engineering and 10 to 14 years of experience in stress analysis or Master's Degree in Mechanical/Aerospace/Applied Mechanics/Structural engineering with 8 to 12 Years of experience.

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