The Temperature and Material Distribution Inside a Gas Turbine Engine

dc.contributor.authorSaraçyakupoğlu, Tamer
dc.date.accessioned2022-02-01T08:37:20Z
dc.date.available2022-02-01T08:37:20Z
dc.date.issued2022en_US
dc.departmentMühendislik ve Mimarlık Fakültesien_US
dc.description.abstractThe propulsion for the air vehicles is generated by the power obtained from the engines. Especially during take-off and climb phases, the air vehicles need the maximum power. Mainly, as presented in Figure 1, it is possible to handle the flight stages in 8 sections, 2 of which are runway maneuvers (Taxi). The cruise phase begins immediately after the climb phase is completed. In this stage, the fuel consumption is less than take-off and climb phases. Although it depends on the aircraft configuration and meteorological conditions, the descent phase, which usually takes place with a 3° nose angle, is one of the most critical stages. In this phase, the use of fuel is less than that of the cruise.en_US
dc.identifier.doi10.31031/EME.2022.04.000576en_US
dc.identifier.issn2640-9690
dc.identifier.issue1en_US
dc.identifier.urihttps://hdl.handle.net/11363/3385
dc.identifier.urihttps://doi.org/
dc.identifier.volume4en_US
dc.institutionauthorSaraçyakupoğlu, Tamer
dc.language.isoenen_US
dc.publisherCrimson Publishersen_US
dc.relation.ispartofEvolutions in Mechanical Engineeringen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectGas turbine engineen_US
dc.subjectMaterial distributionen_US
dc.titleThe Temperature and Material Distribution Inside a Gas Turbine Engineen_US
dc.typeArticleen_US

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