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Innovation Factor

  • Development of an information system with the collection of technical parameters provided by the main manufacturers of gas turbines for aerial propulsion found in existing literature, in order to generate a computational model to be developed in the Python programming language
  • The use of hydrogen as fuel, and its comparative analysis with aviation kerosene, will bring relevant results for the civil aviation segment, both from the perspective of performance of these thermal machines and regarding the combustion of these fuels in gas turbines for aerial propulsion

Advantages of the research line

  • Relevant results for the civil aviation segment, both in the performance of thermal machines and in the combustion of these fuels in gas turbines for aerial propulsion
  • Comparative analysis of the performance of commercial turbines using aviation kerosene with models using hydrogen
  • Promotion of sustainable development in the transportation sector

Segments covered

  • Aviation
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