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ESR 9:
Jan Tomec

My name is Jan Tomec. I am 24 years old and I have just finished my master’s degree in mechanical engineering at the University of Ljubljana. This is also where I finished my bachelor’s degree before that and my high school before that and basically where I lived for the last 10 years. Such monotonous style of life conflicted with my adventurous spirit. The mentor for my internship suggested to me the project THREAD and I was hooked immediately.

For a couple of years now I was working as an intern on different industrial projects which involved mechanics, mathematics and coding. Projects included numerical simulations of nonlinear three-dimensional shell structures, fluid dynamics around rigid bodies, optimisation of production lines and so on. During my studies I took a special interest in continuum mechanics, dynamics, numerical computations and coding.

Considering my background I find the topic on beam theory fascinating. I believe this program will enhance my expertise in the field of mechanics and programming, but also give me a lot of personal experiences. This will give me the edge in the future when I would like to work on similarly engaging projects in industry.


Host Institution
University of Rijeka, Faculty of Civil Engineering (Croatia)
Supervisor

Description

The ESR will work on mechanical analysis of satellite aerials during the rocket-launch phase, when they are exposed to extreme inertial loading and high-frequency vibration and impacts in a compact confinement within a rocket. The design requirement is that the satellite should occupy as little space within the rocket as possible, yet still be able to allow the aerials to deploy without permanent deformation or damage upon satellite ejection from the rocket into the orbit. The simulation will be performed using 1D Cosserat continuum (geometrically exact beam theory) and non-linear finite-element analysis in both statics and dynamics within which various interpolation options will be investigated for accuracy and robustness. In addition, a number of time-stepping schemes will be devised, which shall respect geometry of the problem configuration space and preserve mechanical constants of motion. The work will be supported by an industrial partner in space technologies.

Expected Results

The project is expected to result in higher-order spatial interpolation of displacements and rotations parametrised to provide objective solutions on the non-linear problem manifold. Conservative time-integration techniques devised on different non-linear manifolds will be assessed and generalised to account for unilateral constraints. A test rig will be designed and employed to provide experimental validation.

Secondments