Qualification: ME / M.Tech in Mechanical or Aerospace from a reputed institute
Experience:
10-17 years of experience in the aerospace domain, handling design/analysis projects in the areas of fuselage structures.
Very good knowledge of finite element methods, design calculations (conventional strength of material approach), and hands-on experience in NASTRAN / PATRAN.
A comprehensive knowledge of airframe structural principles and theory.
Excellent knowledge of fatigue and damage tolerance principles and theory is required.
Skills:
Experience in FEA & Stress tools - NASTRAN, PATRAN, HYPERMESH
Fatigue and Damage Tolerance Analysis
Familiarity with aerospace design requirements
MS Office Skills
Excellent communication skills and customer interaction skills. Good verbal and written English skills are essential.
Roles and Responsibilities:
Carry out Finite element analysis for stress, dynamics, and thermal requirements, engineering calculations for the airframe, and jigs & fixtures.
Evaluating material options.
Knowledge and experience of the certification process.
Mass estimation.
Guiding the team for design calculations, best finite element practices.
Knowledge of structural testing (component through to major assemblies).
Manage the team of stress engineers on deliverables, timeline, and performance review.
Provide support to project management.
Interaction with manufacturing agencies/experts to evaluate options.
Creation of technical/design reports/documents.
Interaction with customers to understand their requirements and deliver on time and with quality.
Willingness to travel.
Ottieni una revisione del curriculum gratis e riservata.