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Optimization of combustion and performance parameters by intake-charge conditions in a small-scale air-cooled hydrogen fuelled SI engine suitable for use in piston-prop aircraft

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dc.creator GÜRBÜZ, Habib
dc.date 2020-09-30T21:00:00Z
dc.date.accessioned 2021-01-21T07:55:08Z
dc.date.available 2021-01-21T07:55:08Z
dc.identifier 15ae69a5-91c3-47a7-999f-4ea9525b9e6c
dc.identifier 10.1108/aeat-09-2020-0193
dc.identifier https://avesis.sdu.edu.tr/publication/details/15ae69a5-91c3-47a7-999f-4ea9525b9e6c/oai
dc.identifier.uri http://acikerisim.sdu.edu.tr/xmlui/handle/123456789/78923
dc.description Purpose
dc.language eng
dc.rights info:eu-repo/semantics/closedAccess
dc.title Optimization of combustion and performance parameters by intake-charge conditions in a small-scale air-cooled hydrogen fuelled SI engine suitable for use in piston-prop aircraft
dc.type info:eu-repo/semantics/article


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