IMCS Group
Base pay range
$50.00/hr - $55.00/hr
Job title:
Stress Engineer - Aerospace Duration of the project:
6 Months on W2
Responsibilities
Perform Static, fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
Be familiar with Boeing Static and Book 1,2 and 3 Fatigue Analysis Methodologies.
Use Boeing Stress Tools, including IAS, XSA/SA+, FEADMS, IDTAS, Moss-Duberg, and FAMOSS; understand load paths and extraction of loads from Finite Element Models.
Perform Damage Tolerance Analysis in accordance with CFR 25.571 and determine critical failure modes to ensure structural integrity.
Analyze aircraft primary/secondary metallic structures and read engineering drawings.
Coordinate with cross-functional groups including Design, Materials & Process Engineering.
Participate in review meetings with Customer and SMEs; generate Engineering Stress Reports establishing compliance and safety.
Interact with customers to understand Scope of Work and required methodologies to meet expectations.
Preferred Qualifications
Knowledge of Aerospace industry and standards.
Experience in metallic and composites structural analysis.
Experience in load, stress calculations and preparing technical reports.
Experience in Finite Element Analysis tools (Nastran, Patran).
Experience in static, fatigue and damage tolerance calculations.
Strong oral and written communication skills.
Experience in PATRAN, NASTRAN, FEMAP.
Experience in MRB and SRM.
Experience in CATIA V5, Enovia.
Must have skills
At least bachelor’s degree in mechanical or aerospace engineering.
At least 5 - 12 years of experience in Aerospace Industry as a Stress Engineer.
Comprehensive knowledge of stress analysis of aero structures.
Seniority level
Mid-Senior level
Employment type
Contract
Job function
Information Technology
Industries
Aviation and Aerospace Component Manufacturing and Airlines and Aviation
#J-18808-Ljbffr
Stress Engineer - Aerospace Duration of the project:
6 Months on W2
Responsibilities
Perform Static, fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
Be familiar with Boeing Static and Book 1,2 and 3 Fatigue Analysis Methodologies.
Use Boeing Stress Tools, including IAS, XSA/SA+, FEADMS, IDTAS, Moss-Duberg, and FAMOSS; understand load paths and extraction of loads from Finite Element Models.
Perform Damage Tolerance Analysis in accordance with CFR 25.571 and determine critical failure modes to ensure structural integrity.
Analyze aircraft primary/secondary metallic structures and read engineering drawings.
Coordinate with cross-functional groups including Design, Materials & Process Engineering.
Participate in review meetings with Customer and SMEs; generate Engineering Stress Reports establishing compliance and safety.
Interact with customers to understand Scope of Work and required methodologies to meet expectations.
Preferred Qualifications
Knowledge of Aerospace industry and standards.
Experience in metallic and composites structural analysis.
Experience in load, stress calculations and preparing technical reports.
Experience in Finite Element Analysis tools (Nastran, Patran).
Experience in static, fatigue and damage tolerance calculations.
Strong oral and written communication skills.
Experience in PATRAN, NASTRAN, FEMAP.
Experience in MRB and SRM.
Experience in CATIA V5, Enovia.
Must have skills
At least bachelor’s degree in mechanical or aerospace engineering.
At least 5 - 12 years of experience in Aerospace Industry as a Stress Engineer.
Comprehensive knowledge of stress analysis of aero structures.
Seniority level
Mid-Senior level
Employment type
Contract
Job function
Information Technology
Industries
Aviation and Aerospace Component Manufacturing and Airlines and Aviation
#J-18808-Ljbffr