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dc.contributor.authorTuran, Önder
dc.date.accessioned2019-10-20T19:32:54Z
dc.date.available2019-10-20T19:32:54Z
dc.date.issued2016
dc.identifier.issn1302-3160
dc.identifier.urihttp://www.trdizin.gov.tr/publication/paper/detail/TWpJNE16a3dNQT09
dc.identifier.urihttps://hdl.handle.net/11421/18682
dc.description.abstractThis study investigates energy and entropy analyses of an experimental turbojet engine build in Anadolu University Faculty of Aeronautics and Astronautics Test-Cell Laboratory. Law of motions and Brayton thermodynamic cycle model are used for this purpose. The processes (that is, compression, combustion, and expansion) are simulated in P-v, T-s and h-s diagrams. Furthermore, the second law of thermodynamics is applied to the cycle model to perform the entropy analysis. A distribution of the wasted and thrust power, the overall (energy-based the first law efficiency), and the specific fuel consumption and specific thrust of the engine were calculated during the analyses as well. The results of the study also show the entropy changing value in engine components due to irreversibilities and inefficiencies. As a conclusion, it is expected that this study is useful to study future design and research work similar aircraft turbojets, auxiliary power units and target drone power systems.en_US
dc.description.abstractThis study investigates energy and entropy analyses of an experimental turbojet engine build in Anadolu University Faculty of Aeronautics and Astronautics Test-Cell Laboratory. Law of motions and Brayton thermodynamic cycle model are used for this purpose. The processes (that is, compression, combustion, and expansion) are simulated in P-v, T-s and h-s diagrams. Furthermore, the second law of thermodynamics is applied to the cycle model to perform the entropy analysis. A distribution of the wasted and thrust power, the overall (energy-based the first law efficiency), and the specific fuel consumption and specific thrust of the engine were calculated during the analyses as well. The results of the study also show the entropy changing value in engine components due to irreversibilities and inefficiencies. As a conclusion, it is expected that this study is useful to study future design and research work similar aircraft turbojets, auxiliary power units and target drone power systems.en_US
dc.language.isoengen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectOrtak Disiplinleren_US
dc.titleEnergy and Entropy Analyses of an Experimental Turbojet Engine For Target Drone Applicationen_US
dc.typearticleen_US
dc.relation.journalAnadolu Üniversitesi Bilim ve Teknoloji Dergisi :A-Uygulamalı Bilimler ve Mühendisliken_US
dc.contributor.departmentAnadolu Üniversitesi, Havacılık ve Uzay Bilimleri Fakültesi, Uçak Gövde Motor Bakım Bölümüen_US
dc.identifier.volume17en_US
dc.identifier.issue5en_US
dc.identifier.startpage936en_US
dc.identifier.endpage952en_US
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US]
dc.contributor.institutionauthorTuran, Önder


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