Job Title: Stress Engineer
Location: Richardson TX (Onsite)
Duration: 6 Months
Implementation Partner: Kaleidoscope Innovation
End Client: To be disclosed
Job Description:
- Perform Static fatigue and damage tolerance analysis for Aircraft structures
- Use of classical hand calculation approach to analyze both primary and secondary structures
- Understanding of load paths extraction of loads from Finite Element Models
- Determination of critical failure modes and performing analysis to ensure structural integrity
- Analysis of both metallic & composite structures
- Determination of dispositions for structural non conformances
- Coordinate with cross functional groups including Design Materials & Process Engineering Manufacturing Engineering Liaison Engineering and on
- Participate in review meetings with Customer and Suppliers
- Engineering Stress report generation and review
- Interact with customer; prepare Scope of Work laydown the execution methodology to ensure that the projects executed meet the customer requirements
Required Qualifications (Nonnegotiable requirements):
- At least Bachelors degree in Mechanical or Aerospace engineering
- At least 5 years (< 18years) of experience in Aerospace Industry as a Stress Engineer
- Comprehensive knowledge Stress analysis of Aero structures
- Having Hands on experience in one or more Finite Element Post Processing Tools (e.g. PATRAN)
Preferred Qualifications:
- Experience in providing technical solutions from conceptual to detailed design stage
- Use of Finite Element Methods for load extraction and to solve complex engineering problems
- Experience in performing Fatigue and Damage Tolerance Analysis
- Working knowledge of Boeing standards
- Working knowledge of Code of Federal Regulations Title 14 Part 25
- Experienced in PATRAN NASTRAN FEMAP
- Experience in CATIA V5 Enovia
- Strong oral and written communication skills