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dc.contributor.authorCavcar, Mustafa
dc.contributor.authorCavcar, Aydan
dc.date.accessioned2019-10-22T20:07:01Z
dc.date.available2019-10-22T20:07:01Z
dc.date.issued2003
dc.identifier.isbn9781563479458 -- 9781624100895
dc.identifier.urihttps://hdl.handle.net/11421/22169
dc.descriptionAIAA Atmospheric Flight Mechanics Conference and Exhibit 2003 -- 11 August 2003 through 14 August 2003 -- Austin, TX -- 103004en_US
dc.description.abstractA set of aircraft performance figures of merit for different phases of flight mission is derived from aircraft performance equations. In addition, an overall performance figure of merit combining the derived performance figures of merit is introduced. Presented performance figures of merit can be used in comparison of the turbojet/fan transport aircraft performance. The derived figures of merit can be calculated from published data of existing aircraft. In addition, a method to predict aerodynamic and propulsion characteristics of a given aircraft is introduced. Moreover, an application of the usage of performance figures of merit in conceptual design of new aircraft is presenteden_US
dc.language.isoengen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titlePerformance figures of merit for turbojet/fan transport aircraft performance comparison and conceptual designen_US
dc.typeconferenceObjecten_US
dc.relation.journalAIAA Atmospheric Flight Mechanics Conference and Exhibiten_US
dc.contributor.departmentAnadolu Üniversitesi, Sivil Havacılık Yüksekokuluen_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US]
dc.contributor.institutionauthorCavcar, Mustafa
dc.contributor.institutionauthorCavcar, Aydan


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