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Constant Altitude-Constant Mach Number Cruise Range of Transport Aircraft with Compressibility Effects

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dc.contributor.authorCavcar, Aydan
dc.date.accessioned2025-11-13T10:49:18Z
dc.date.issued2006-01-01
dc.identifier.doihttps://doi.org/10.2514/1.14252
dc.identifier.endpage131
dc.identifier.issn0021-8669
dc.identifier.issue1
dc.identifier.openalexW2130164900
dc.identifier.startpage125
dc.identifier.urihttps://hdl.handle.net/11421/5358
dc.identifier.urihttps://doi.org/10.2514/1.14252
dc.identifier.volume43
dc.language.isoen
dc.relation.ispartofJournal of Aircraft
dc.rightsrestrictedAccess
dc.subjectMach number
dc.subjectConstant (computer programming)
dc.subjectCruise
dc.subjectAerospace engineering
dc.subjectCompressibility
dc.subjectRange (aeronautics)
dc.subjectAltitude (triangle)
dc.subjectMechanics
dc.subjectPhysics
dc.subjectEnvironmental science
dc.subjectMeteorology
dc.subjectMathematics
dc.subjectGeometry
dc.subjectEngineering
dc.subjectComputer science
dc.subject.sdg7
dc.titleConstant Altitude-Constant Mach Number Cruise Range of Transport Aircraft with Compressibility Effects
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5023712238

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