Stress Engineer

Richardson, TX

Contract Position

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

7Co-ordinate 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

At least Bachelor’s 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