Job Title: Stress Engineer Aerospace
Work Location: Richardson TX 75082 or Wichita KS (Day One Onsite)
Duration: Long Term
Must Have:
- CATIA V5 Enovia CFR25.571
- Minimum years of experience required: 5-12 Years
- At least bachelors degree in mechanical or aerospace engineering
- At least 5 years (< 12years) of experience in Aerospace Industry as a Stress Engineer
- Comprehensive knowledge Stress analysis of Aero structures.
- Boeing Stress Tools including IAS XSA/SA FEADMS IDTAS Moss-Duberg and FAMOSS Understanding of load paths extraction of loads from Finite Element Models.
- Experienced in PATRAN NASTRAN FEMAP
Detailed Job Description:
- Perform Static fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
- Applicant should be familiar with Boeing Static and Book 12 and 3 Fatigue Analysis Methodologies
- Applicant should be familiar with and have prior experience with the following Boeing Stress Tools including IAS XSA/SA FEADMS IDTAS Moss-Duberg and FAMOSS Understanding of load paths extraction of loads from Finite Element Models.
- Applicant should be familiar with Damage Tolerance Analysis and CFR25.571
- Determination of critical failure modes and performing analysis to ensure structural integrity.
- Analysis of aircraft primary/secondary metallic structures.
- Read and interpret engineering drawings.
- Coordinate with cross functional groups including Design Materials & Process Engineering.
- Participate in review meetings with Customer and SMEs.
- Generate Engineering Stress Report which establishes compliance and safety.
- Interact with customer; understand the Scope of Work and methodology required to meet customer expectations
Job Title: Stress Engineer Aerospace Work Location: Richardson TX 75082 or Wichita KS (Day One Onsite) Duration: Long Term Must Have: CATIA V5 Enovia CFR25.571 Minimum years of experience required: 5-12 Years At least bachelors degree in mechanical or aerospace engineering At least 5 years ...
Job Title: Stress Engineer Aerospace
Work Location: Richardson TX 75082 or Wichita KS (Day One Onsite)
Duration: Long Term
Must Have:
- CATIA V5 Enovia CFR25.571
- Minimum years of experience required: 5-12 Years
- At least bachelors degree in mechanical or aerospace engineering
- At least 5 years (< 12years) of experience in Aerospace Industry as a Stress Engineer
- Comprehensive knowledge Stress analysis of Aero structures.
- Boeing Stress Tools including IAS XSA/SA FEADMS IDTAS Moss-Duberg and FAMOSS Understanding of load paths extraction of loads from Finite Element Models.
- Experienced in PATRAN NASTRAN FEMAP
Detailed Job Description:
- Perform Static fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
- Applicant should be familiar with Boeing Static and Book 12 and 3 Fatigue Analysis Methodologies
- Applicant should be familiar with and have prior experience with the following Boeing Stress Tools including IAS XSA/SA FEADMS IDTAS Moss-Duberg and FAMOSS Understanding of load paths extraction of loads from Finite Element Models.
- Applicant should be familiar with Damage Tolerance Analysis and CFR25.571
- Determination of critical failure modes and performing analysis to ensure structural integrity.
- Analysis of aircraft primary/secondary metallic structures.
- Read and interpret engineering drawings.
- Coordinate with cross functional groups including Design Materials & Process Engineering.
- Participate in review meetings with Customer and SMEs.
- Generate Engineering Stress Report which establishes compliance and safety.
- Interact with customer; understand the Scope of Work and methodology required to meet customer expectations
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