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Comparison of Generalized Approximate Cruise Range Solutions for Turbojet/Fan Aircraft

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dc.contributor.authorCavcar, Mustafa
dc.contributor.authorCavcar, Aydan
dc.date.accessioned2025-11-13T11:16:41Z
dc.date.issued2003-09-01
dc.identifier.doihttps://doi.org/10.2514/2.6879
dc.identifier.endpage895
dc.identifier.issn0021-8669
dc.identifier.issue5
dc.identifier.openalexW2012180120
dc.identifier.startpage891
dc.identifier.urihttps://hdl.handle.net/11421/6273
dc.identifier.urihttps://doi.org/10.2514/2.6879
dc.identifier.volume40
dc.language.isoen
dc.relation.ispartofJournal of Aircraft
dc.rightsrestrictedAccess
dc.subjectMach number
dc.subjectCruise
dc.subjectAirspeed
dc.subjectAerospace engineering
dc.subjectWing
dc.subjectTurbojet
dc.subjectFuel efficiency
dc.subjectDrag
dc.subjectConstant (computer programming)
dc.subjectRange (aeronautics)
dc.subjectDrag divergence Mach number
dc.subjectAngle of attack
dc.subjectRamjet
dc.subjectMechanics
dc.subjectAerodynamics
dc.subjectPhysics
dc.subjectDrag coefficient
dc.subjectEngineering
dc.subjectComputer science
dc.subject.sdg7
dc.titleComparison of Generalized Approximate Cruise Range Solutions for Turbojet/Fan Aircraft
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5082535208
local.authorid.openalexA5023712238

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