Student Theses

Here you will find information about currently available thesis topics at the Institute of Aircraft Structures

In the following sections, you will find the thesis opportunities currently available at the IFB. If you are interested, please contact the person listed for each opportunity. Please include a current academic transcript, a brief CV, and your preferred start date in your message.

Bachelor's Thesis Opportunities at the IFB

In resin transfer molding (RTM), local variations in the permeability of the semi-finished fiber material lead to different flow front profiles—despite identical process boundary conditions—and thus to dry spots and pores. Data-driven models can predict the filling process and serve as the basis for process control (see Figure 1). However, this requires extensive, time-synchronized, and uniformly processed measurement data. The institute has an RTM plate mold with glass halves available, in which the filling process can be directly observed optically.

The goal of this work is to develop a camera-based measurement system that captures the flow front in the transparent mold in real time and evaluates it automatically. The image data, together with other process variables (e.g., injection pressure, temperature), will be made available via the institute’s IIoT infrastructure so that the resulting datasets can be immediately used for the training and validation of machine learning models for flow front prediction.

Type: Bachelor Thesis
Organisation: Aircraft Design (060310)
Supervisor:
Examiner: Michael May
Link: To C@MPUS

Type: Bachelor Thesis
Organisation: Aircraft Design (060310)
Supervisor:
Examiner: Michael May
Link: To C@MPUS

Since 2008, the InVentus team has been developing and operating a headwind vehicle. This is a vehicle that uses wind turbines exclusively as its power source for propulsion. Together with other student teams from around the world, InVentus participates in “Racing Aeolus,” an international competition held annually in August on the coast of the Netherlands near the city of Den Helder.

In addition to the main mechanical turbine, the InVentus team plans to install a second, smaller turbine at the front of the vehicle. Previous research has shown that the optimal hub height of the front turbine depends on the wind direction. The goal of this thesis is to redesign the yaw system and the mast so that the height of the front turbine can be adjusted. At the same time, the design should allow for quick disassembly of the turbine so that the vehicle can be switched between configurations with one or both turbines. To this end, requirements will first be gathered, and potential solutions will be discussed and evaluated in order to develop a concept. The concept will then be implemented in CAD and sized.

Type: Bachelor Thesis
Organisation: Aircraft Design (060300)
Supervisor:
Examiner: Andreas Strohmayer
Link: To C@MPUS

Master's Thesis Opportunities at the IFB

Within this thesis, an existing test platform will be further developed from a design perspective and qualified for thermal measurements. Using controllable and interchangeable heat sources, suitable thermal insulation, as well as infrared and heat flux sensors, temperature fields, heat fluxes, and effective thermal resistances of different plate specimens will be investigated. Particular challenges include reproducible contact pressure, thermal contact and interface resistances, and parasitic heat losses. These effects will be evaluated using suitable reference materials and specimens of different thicknesses.

The infrared camera will be used both for full-field measurements and, in combination with a microscope lens, for high-resolution investigations of specimen cross-sections. This includes the determination of effective emissivities for quantitative infrared measurements and the development of an optical access through the thermal insulation. In addition, image shifts caused by vibrations from the camera’s internal cooling system are to be reduced mechanically and, if required, digitally. Finally, the test platform will be validated using reference and composite specimens and applied to stationary and transient thermal measurements. Advanced thermographic methods such as lock-in thermography may also be investigated

Type: Master Thesis
Requirement: Independent working style, engineering design skills, programming experience
Acquirement: • Literature review and familiarization with the topic
• Design and further development of the modular test setup
• Integration and calibration of the measurement systems
• Mechanical and, if required, digital image stabilization
• Validation and execution of thermal measurements
• Data evaluation and documentation
Organisation: Aircraft Design (060310)
Supervisor:
Examiner: Stefan Carosella
Michael May
Link: To C@MPUS

In this work the student will adapt previous code developed at the university of Zurich and available open access to floating wind farms. The activity will be performed with the support of the supervisor and direct collaboration with ETH, which will provide theoretical and coding support.

Type: Master Thesis
Organisation: Aircraft Design (060300)
Supervisor:
Examiner: Po Wen Cheng
Link: To C@MPUS

Floating offshore wind turbines will allow the exploitation of the wind energy resource even in deep waters. Currently, there are still significant open challenges to reduce the cost associated with floating wind turbines and allow the commercialization of the technology. Among them, improved methodologies are required to correctly estimate the loading on the mooring system used for station keeping of the machines. In fact, the mooring lines are currently designed following standard practices from the Oil and Gas industry, leading to significant overestimation and costs. To reduce uncertainty in the design process and reduce costs, improved knowledge on the loading and fatigue are required; however, numerical models are usually computationally expensive, as a significant number of operating conditions and system designs need to be tested to identify an optimal solution. In this framework, machine learning methods can be exploited to develop a model for predicting mooring line fatigue, without the need for computationally expensive simulations. The model can then be leveraged to optimize the design by comparing large numbers of technical solutions at a fraction of the cost.

Objectives
1. Adapt current machine learning python libraries for the assessment of fatigue loading
2. Test different algorithms identified in the literature (linear regression, graph based neural networks, etc) to assess the models that provide the best performance

Recommended workflow
1 Review of current design standards and workflows for design of mooring lines in floating wind
The first task will involve reviewing existing literature concerning the design of mooring lines for floating wind turbines. The student will be guided in this taks, learning about how to perform a critical review of the literature following scientific and technical standards exploiting available software and databases for literature review. This part of the work will leverage also previous work from other students, limiting the required effort and time expense.
2 Adaptation of available machine learning models for fatigue prediction for mooring lines
Currently multiple machine learning models have been proposed in the literature to tackle a vast variety of problems. Such models, developed by software engineers, have been mostly structured into open-access python libraries, which can be freely used and adapted by any user. In this step, the student will learn about one of this libraries (possibly pytorch) and apply it for the prediction of fatigue loading.

3 Assessment of different machine learning algorithm
The python library selected within the scope of the thesis will be used to benchmark different machine learning algorithms. The student will use floating wind turbine data already structured and post-processed to train different algorithms and assess their performance. User-defined parameters will be investigated to perform a sensitivity of results to different setups.

Type: Master Thesis
Requirement: • Some basic knowledge about programming (especially python)
• Basic knowledge about wind energy
• Basic knowledge about mechanical design (fatigue load calculation)
Acquirement: • Post-process wind turbine simulation data
• Train relevant machine learning models
• Assess quality of results and validation of models
Organisation: Aircraft Design (060300)
Supervisor:
Examiner: Po Wen Cheng
Link: To C@MPUS

The aim of this work is to investigate the applicability of the SimTex FE solver, a solver optimized for contact-intensive, multi-fiber-based simulation models, to the numerical simulation of the coreless filament winding manufacturing process, as well as a downstream expansion-based modeling strategy to consider fiber bundle deformation. Within the scope of the thesis, a Python-based optimization workflow with pre- and post-processors for modeling and evaluation will be expanded and used as the basis for parameter studies and parameter calibration using small reference structures. The results will then be analyzed with regard to the limitations of the modeling approach, the computation time, and deviations from geometric measurement data of corresponding measurement of test specimens.

Work Packages:
- Literature review and induction (Coreless filament winding (CFW), textile submesoscopic multifilament modeling strategies)
- Investigation of the suitability of the SimTex solver for the problem
- Advancement of a pre- and postprocessor for modeling and calibration
- Investigation of parameters affecting the modeling results and calibration
- Validation of the geometrical results against existing experimental data
- Documentation and presentation of the results

Type: Master Thesis
Organisation: Aircraft Design (060300)
Supervisor:
Examiner: Michael May
Link: To C@MPUS

Auxetic structures are characterized by a negative transverse contraction coefficient and exhibit exceptional mechanical properties such as increased energy absorption and dissipation, improved damage resistance, and adaptable stiffness behavior. While auxetic lattice structures have been studied predominantly in isotropic materials, their combination with anisotropic fiber composites has not yet been sufficiently researched.
The aim of this work is to design, manufacture, and experimentally investigate an auxetic lattice structure made of a fiber composite material. These lattice structures are to be placed in the context of engine suspension for rear-mounted engines in novel aircraft designs. The focus is on analyzing the mechanical behavior under quasi-static loading and the vibration characteristics of the structure in order to evaluate the potential of auxetic FRP lattices for lightweight design.

Type: Master Thesis
Organisation: Aircraft Design (060310)
Supervisor:
Examiner: Stefan Carosella
Link: To C@MPUS

Unsolicited Applications

If no thesis projects are listed, unfortunately there are currently no topics available. However, you are welcome to contact the department heads at any time to express your interest in a thesis project.

Please briefly describe your academic interests and include your current academic transcript, a brief CV, and your preferred start date in your message.

Similarity Mechanics and Design Theory

Manufacturing Technology

Aircraft Design

Lightweight Construction and Simulation

Wind Energy

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