Gelişmiş Arama

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dc.contributor.authorŞöhret, Yasin
dc.contributor.authorEkici, Selçuk
dc.contributor.authorKarakoç, Tahir Hikmet
dc.date.accessioned2019-10-20T19:32:45Z
dc.date.available2019-10-20T19:32:45Z
dc.date.issued2018
dc.identifier.issn0360-3199
dc.identifier.issn1879-3487
dc.identifier.urihttps://dx.doi.org/10.1016/j.ijhydene.2017.12.060
dc.identifier.urihttps://hdl.handle.net/11421/18632
dc.descriptionWOS: 000436225600035en_US
dc.description.abstractRamjet engines are widely-used devices in the defence industry and have military applications. These engine types, preferred in many fields, are known to act according to the laws of thermodynamics. For this reason, exergy analysis methodology is a beneficial tool for assessing the performance of a ramjet engine, as well as other energy conversion systems. The present study aims to introduce a performance analysis of a hydrogen fueled ramjet engine within the framework of the first and second laws of thermodynamics. At the end of the study, the exergy efficiencies of inlet, combustion zone and nozzle are found to be 3.88%, 7.62%, and 0.03%, respectively, whereas the exergy efficiency of a ramjet engine is 8.85%. The introduced methodology and the results obtained from the current study may be useful for anybody who is interested in thermal sciences and aero-propulsion technologies.en_US
dc.description.sponsorshipAnadolu University [1404F237]; Suleyman Demirel Universityen_US
dc.description.sponsorshipThis study was funded by Anadolu University (Grant No. 1404F237). The authors are thankful to Anadolu and Suleyman Demirel Universities for their support and thank the reviewers for their valuable comments and contribution to the improvement and quality of the paper.en_US
dc.language.isoengen_US
dc.publisherPergamon-Elsevier Science LTDen_US
dc.relation.isversionof10.1016/j.ijhydene.2017.12.060en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAlternative Fuelen_US
dc.subjectCycle Analysisen_US
dc.subjectExergyen_US
dc.subjectHydrogenen_US
dc.subjectRamjeten_US
dc.subjectThermodynamicsen_US
dc.titleUsing exergy for performance evaluation of a conceptual ramjet engine burning hydrogen fuelen_US
dc.typearticleen_US
dc.relation.journalInternational Journal of Hydrogen Energyen_US
dc.contributor.departmentAnadolu Üniversitesi, Havacılık ve Uzay Bilimleri Fakültesi, Uçak Gövde Motor Bakım Bölümüen_US
dc.identifier.volume43en_US
dc.identifier.issue23en_US
dc.identifier.startpage10842en_US
dc.identifier.endpage10847en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US]
dc.contributor.institutionauthorKarakoç, Tahir Hikmet


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