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Parallel Solution of Low Aspect Ratio Rectangular Flat Wings in Compressible Flow

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dc.contributor.authorDurmuş, Gökhan
dc.contributor.authorMehmet Şerif Kavsaoğlu
dc.contributor.authorÜnver Kaẏnak
dc.contributor.orcid0000-0002-8382-3576
dc.date.accessioned2025-11-13T21:30:03Z
dc.date.issued2005-01-10
dc.identifier.doihttps://doi.org/10.2514/6.2005-1224
dc.identifier.openalexW2327418912
dc.identifier.urihttps://hdl.handle.net/11421/13653
dc.identifier.urihttps://doi.org/10.2514/6.2005-1224
dc.language.isoen
dc.relation.ispartof43rd AIAA Aerospace Sciences Meeting and Exhibit
dc.rightsrestrictedAccess
dc.subjectAspect ratio (aeronautics)
dc.subjectFlow (mathematics)
dc.subjectMechanics
dc.subjectCompressibility
dc.subjectCompressible flow
dc.subjectMaterials science
dc.subjectGeometry
dc.subjectPhysics
dc.subjectMathematics
dc.subjectComposite material
dc.subject.sdg11
dc.titleParallel Solution of Low Aspect Ratio Rectangular Flat Wings in Compressible Flow
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5049179266

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