⚠️Only available for residents of Red Oak, TX, USA⚠️
Our client is a multinational company specializing in information technology (IT), business process outsourcing (BPO), and consulting services.
Global Presence: Operates in over 90 countries with delivery centers worldwide.
Employees: Over 160,000 professionals globally.
Services and Offerings
- IT Services: Software development, IT consulting, cloud services, data analytics, and cybersecurity.
- Digital Transformation: AI/ML integration, IoT solutions, and blockchain services.
- Telecom Solutions: A significant focus area, including 5G technology and network transformation.
- Enterprise Solutions: ERP (Enterprise Resource Planning) systems, CRM (Customer Relationship Management), and supply chain solutions.
- BPO Services: Customer service, finance and accounting outsourcing, and HR services.
The company is known for its innovation in digital transformation, cloud computing, and AI-driven solutions.
Key Partnerships
Strategic alliances with companies such as:
- Microsoft
- Amazon Web Services (AWS)
- Google Cloud
- SAP
- Oracle
Job Title: Stress Engineer
Location: Red Oak, Texas
Onsite/ Remote: Day 1 Onsite at customer location
Full time: $105k
Subcon: 58/hr
Acceptable Visa: USC/GC/H1B (No transfer)
JD:
- Perform sizing and support analysis activities for design changes, improvements, and new aircraft development programs.
- Support the design process from initial concept through final production, ensuring the aircraft meets or exceeds all technical requirements.
- Support different teams to ensure a quality product with supporting documentation are produced.
- Write structural substantiation reports, that meet technical compliance to program, and certifying authority, requirements and guidelines.
- Create new and/or update existing certification Detail Finite Element
- Models.
How to thrive in this role?
You possess a B.S. in Aerospace, Mechanical or Civil Engineering from an accredited university.
You have a minimum of five (5) years of experience in aircraft structural substantiation analysis.
You have proficiency in classical stress (static) analysis methods.
You have a proficiency and experience in Fatigue and Damage Tolerance (F&DT) analysis methods and tools (i.e Nasgro).
You have proficiency in classical analysis methods.
You have proficiency in FEM based analysis tools (MSC Patran/Nastran, Altair Hypermesh) developing/running DFEMs and also GFEMs (loads models).
You have knowledge of interactions between loads and structures.
You have knowledge and experience of structural sizing methodologies.
You have an understanding of civil aircraft certification rules and experience in certification procedures.
You have proficiency with CATIA V5, Enovia applications – preferred.