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Student (f/m/x) - Analysis and Development of Generic Reference Models for AFP Components

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Onsite

Student (f/m/x) - Analysis and Development of Generic Reference Models for AFP Components

German Aerospace Center (DLR)

Student (f/m/x) - Analysis and Development of Generic Reference Models for AFP Components

20 days ago

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Important information


Contract type:

Permanent

Location:

21 Stade, Germany

Work mode:

Onsite

Published on:

8 October 2026

What they need


Would you like to become part of our innovation-driven research team and help shape the future of lightweight system? We, the Institute of Lightweight Systems, develop and test new lightweight construction technologies for resource-saving and climate-friendly structures in the aerospace, transport, energy and security sectors. Our vision is intelligent lightweight system construction for an emission-free tomorrow.

What To Expect Automated Fiber Placement (AFP) is a key technology for the efficient manufacturing of complex composite structures in aerospace applications. Representative component models that capture the characteristic features of real aircraft structures are essential for investigating and evaluating different manufacturing concepts.

As part of your thesis, you will analyze typical aerospace composite components and develop generic reference models based on their characteristic features. These models will serve as a foundation for future investigations and comparative assessments of AFP manufacturing processes. You will gain insights into the structural design of composite components, automated fiber placement, and the development of representative component models for manufacturing process evaluation.

Your tasks

  • Research and analyze AFP-relevant composite components used in aircraft structures
  • Identify and systematically document characteristic structural and laminate features, such as fiber orientation distributions, laminate thicknesses, and the type, proportion, and distribution of local reinforcements (patches)
  • Derive representative component characteristics and define suitable generic reference structures
  • Develop and model the reference structures, including their laminate layups, using CAD/CPD software
  • Document the underlying assumptions, modeling approaches, and results

Your profile

  • Currently enrolled in a degree program in aerospace engineering, mechanical engineering, materials science, or a related field
  • Basic knowledge of composite materials, particularly laminate design and structural behavior
  • Initial experience with CAD modeling, ideally using CATIA CPD
  • Structured and independent approach to work
  • Analytical thinking skills
  • Very good written and spoken German and/or English skills

We look forward to getting to know you!

If you have any questions about this position ( Vacancy-ID 6454 ) please contact:

Dominik Delisle Tel.: +49 531 295-3738

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