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Development of concepts for detecting hydrogen micro flames. - programming a thermodynamical simulation tool for hydrogen micro flames (including a graphical user interface)- definition and collection of aviation-specific requirements for novel detection concepts by means of literature/norm review and expert interviews- inventing novel detection concepts (multiple concepts are now patent pending)- performing a risk assessment for the best concepts- performing design considerations for the finally best concept- development and building of a test rig for producing and analyzing small hydrogen flames - experiment based assessment of the novel detection concepts and validation of the simulation model- building a proof-of-concept for the best novel detection concept

Designing and numerically optimizing liquid hydrogen tanks for aircraft applications by thermal and mechanical means. Researching for novel thermal insulation concepts.

In a team of 5 students, we developed and experimentally validated a protocol for determining the flight quality of a quadrocopter drone as part of the PIE of the ISAE Supaéro (project of engineering and entrepreneurship).

Modeling and numerically optimizing hydrogen system architectures for fuel cell based aircraft- development of hydrogen system architectures - performing numerical system optimization for the developed architectures

Thermodynamic modeling and analysis of liquid hydrogen tank thermal insulation concepts for aviation applications - Junior Research Group SE2A (Excellence Cluster Sustainable and Energy-Efficient Aviation)

Further development of the demonstrator for a fuel cell-based propulsion engine for aviation (small-scale - 12 kW / 16 PS)

Development and building of a demonstrator for a fuel cell-based propulsion engine for aviation (small-scale - 12 kW / 16 PS)

Development of fuel cell systems for an octocopter drone application.