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Unsteady Navier Stokes Solutions of Low Aspect Ratio Rectangular Flat Wings in Compressible Flow

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dc.contributor.authorGökhan Durmuş
dc.contributor.authorDurmuş, Gökhan
dc.contributor.authorMehmet Şerif Kavsaoğlu
dc.contributor.authorKavsaoğlu, Mehmet Şerif
dc.contributor.authorÜnver Kaẏnak
dc.contributor.orcid0000-0002-8382-3576
dc.date.accessioned2025-11-13T21:26:09Z
dc.date.issued2008-02-04
dc.identifier.doihttps://doi.org/10.1007/978-3-540-92744-0_37
dc.identifier.endpage304
dc.identifier.issn1439-7358
dc.identifier.openalexW934297903
dc.identifier.startpage297
dc.identifier.urihttps://hdl.handle.net/11421/13413
dc.identifier.urihttps://doi.org/10.1007/978-3-540-92744-0_37
dc.language.isoen
dc.relation.ispartofLecture notes in computational science and engineering
dc.rightsrestrictedAccess
dc.subjectTransonic
dc.subjectAspect ratio (aeronautics)
dc.subjectVortex
dc.subjectDelta wing
dc.subjectMechanics
dc.subjectLeading edge
dc.subjectSuction
dc.subjectFlow (mathematics)
dc.subjectEnhanced Data Rates for GSM Evolution
dc.subjectWind tunnel
dc.subjectBubble
dc.subjectAngle of attack
dc.subjectCompressibility
dc.subjectPhysics
dc.subjectGeometry
dc.subjectMathematics
dc.subjectEngineering
dc.subjectAerodynamics
dc.subjectMeteorology
dc.subject.sdg7
dc.titleUnsteady Navier Stokes Solutions of Low Aspect Ratio Rectangular Flat Wings in Compressible Flow
dc.typebook-chapter
dspace.entity.typePublication
local.authorid.openalexA5049179266
local.authorid.openalexA5042277913

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