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THEORETICAL INVESTIGATION OF ROCKET ENGINES FOR OXYGEN AND ETHANE LIQUID BIPROPELLANT

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cris.virtual.department#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtual.orcid#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtualsource.department3fade673-6db4-4e4b-a77c-0b1e7e3b5f6e
cris.virtualsource.orcid3fade673-6db4-4e4b-a77c-0b1e7e3b5f6e
dc.contributor.authorNevsan Sengil
dc.date.accessioned2024-05-23T11:32:35Z
dc.date.available2024-05-23T11:32:35Z
dc.date.issued2021-11-10
dc.identifier.doi10.17654/0973576321006
dc.identifier.urihttps://acikarsiv.thk.edu.tr/handle/123456789/154
dc.publisherPushpa Publishing House
dc.relation.ispartofJP Journal of Heat and Mass Transfer
dc.relation.issn0973-5763
dc.titleTHEORETICAL INVESTIGATION OF ROCKET ENGINES FOR OXYGEN AND ETHANE LIQUID BIPROPELLANT
dc.typejournal-article
dspace.entity.typePublication
oaire.citation.issue2
oaire.citation.volume24

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