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dc.contributor.authorUhlár, Erik
dc.contributor.authorČerňan, Jozef
dc.date.accessioned2021-06-18T10:45:17Z
dc.date.available2021-06-18T10:45:17Z
dc.date.issued2021
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/420
dc.description.abstractIn order to help accelerate transition to sustainable and eco-friendly personal transportation in a single engine piston aircraft category we’ve developed a simulation software platform of hydrogen powered aircraft for further research and development. Measurements were carried out on a real reference airplane Cessna 172 R and were crosschecked with an airplane flight manual as well as a computer flight simulation. We also focused on a software-based safety and economy optimization by components usage ratio improvement and inflight energy production and transfer limitations.en_US
dc.language.isosken_US
dc.publisherUniversity of Zilinaen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectHydrogen fuel cellen_US
dc.subjectCompressed gaseous hydrogenen_US
dc.subjectElectric airplane propulsionen_US
dc.titleSystem optimization demonstrator for aircraft propulsion technology using fuel cellsen_US
dc.typeConference paperen_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2021.1.29


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Except where otherwise noted, this item's license is described as http://creativecommons.org/licenses/by/4.0/