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Optimum Range and Endurance of a Piston Propeller Aircraft with Cambered Wing

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dc.contributor.authorCavcar, Mustafa
dc.contributor.authorCavcar, Aydan
dc.date.accessioned2025-11-13T11:18:01Z
dc.date.issued2005-01-01
dc.identifier.doihttps://doi.org/10.2514/1.6095
dc.identifier.endpage217
dc.identifier.issn0021-8669
dc.identifier.issue1
dc.identifier.openalexW1987158222
dc.identifier.startpage212
dc.identifier.urihttps://hdl.handle.net/11421/6349
dc.identifier.urihttps://doi.org/10.2514/1.6095
dc.identifier.volume42
dc.language.isoen
dc.relation.ispartofJournal of Aircraft
dc.rightsrestrictedAccess
dc.subjectWing
dc.subjectPropeller
dc.subjectAeronautics
dc.subjectPiston (optics)
dc.subjectRange (aeronautics)
dc.subjectWing loading
dc.subjectWing configuration
dc.subjectAerospace engineering
dc.subjectAngle of attack
dc.subjectMarine engineering
dc.subjectSwept wing
dc.subjectEngineering
dc.subjectAerodynamics
dc.subjectAutomotive engineering
dc.subjectStructural engineering
dc.subjectPhysics
dc.subject.sdg7
dc.titleOptimum Range and Endurance of a Piston Propeller Aircraft with Cambered Wing
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5082535208
local.authorid.openalexA5023712238

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