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16.100 Aerodynamics, Fall 2002

dc.contributor.authorDarmofal, David L.en_US
dc.coverage.temporalFall 2002en_US
dc.date.issued2002-12
dc.identifier16.100-Fall2002
dc.identifierlocal: 16.100
dc.identifierlocal: IMSCP-MD5-ca5af9d3a64264f3b80e7f6ceb8a8775
dc.identifier.urihttp://hdl.handle.net/1721.1/36884
dc.description.abstractThis course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub/supersonic regimes. 16.100 generally has four components: subsonic potential flows, including source/vortex panel methods; viscous flows, including laminar and turbulent boundary layers; aerodynamics of airfoils and wings, including thin airfoil theory, lifting line theory, and panel method/interacting boundary layer methods; and supersonic and hypersonic airfoil theory. Course material varies each year depending upon the focus of the design problem.en_US
dc.languageen-USen_US
dc.rights.uriUsage Restrictions: This site (c) Massachusetts Institute of Technology 2003. Content within individual courses is (c) by the individual authors unless otherwise noted. The Massachusetts Institute of Technology is providing this Work (as defined below) under the terms of this Creative Commons public license ("CCPL" or "license"). The Work is protected by copyright and/or other applicable law. Any use of the work other than as authorized under this license is prohibited. By exercising any of the rights to the Work provided here, You (as defined below) accept and agree to be bound by the terms of this license. The Licensor, the Massachusetts Institute of Technology, grants You the rights contained here in consideration of Your acceptance of such terms and conditions.en_US
dc.subjectaerodynamicsen_US
dc.subjectairflowen_US
dc.subjectairen_US
dc.subjectbodyen_US
dc.subjectaircraften_US
dc.subjectaerodynamic modesen_US
dc.subjectaeroen_US
dc.subjectforcesen_US
dc.subjectCFDen_US
dc.subjectaerodynamic analysisen_US
dc.subjectliften_US
dc.subjectpotential flowsen_US
dc.subjectsupersonicen_US
dc.subjectsubsonicen_US
dc.subjectpanel methoden_US
dc.subjectvortex lattice methoden_US
dc.subjectboudary layeren_US
dc.subjecttransitionen_US
dc.subjectturbulenceen_US
dc.subjectinvisciden_US
dc.subjectviscousen_US
dc.subjecteuleren_US
dc.subjectnavier-stokesen_US
dc.subjectwind tunnelen_US
dc.subjectflow similarityen_US
dc.subjectnon-dimensionalen_US
dc.subjectmach numberen_US
dc.subjectreynolds numberen_US
dc.subjectintegral momentumen_US
dc.subjectairfoilen_US
dc.subjectstallen_US
dc.subjectfriction dragen_US
dc.subjectdragen_US
dc.subjectinduced dragen_US
dc.subjectwave dragen_US
dc.subjectpressure dragen_US
dc.subjectfluid elementen_US
dc.subjectshear strainen_US
dc.subjectnormal strainen_US
dc.subjectvorticityen_US
dc.subjectdivergenceen_US
dc.subjectsubstantial derviativeen_US
dc.subjectlaminaren_US
dc.subjectdisplacement thicknessen_US
dc.subjectmomentum thicknessen_US
dc.subjectskin frictionen_US
dc.subjectseparationen_US
dc.subjectvelocity profileen_US
dc.subject2-d panelen_US
dc.subject3-d vortexen_US
dc.subjectthin airfoilen_US
dc.subjectlifting lineen_US
dc.subjectaspect ratioen_US
dc.subjecttwisten_US
dc.subjectcamberen_US
dc.subjectwing loadingen_US
dc.subjectroll momentsen_US
dc.subjectfinite volume approximationen_US
dc.subjectshocksen_US
dc.subjectexpansion fansen_US
dc.subjectshock-expansion theoryen_US
dc.subjecttransonicen_US
dc.subjectcritical mach numberen_US
dc.subjectwing sweepen_US
dc.subjectKutta conditionen_US
dc.subjectteam projecten_US
dc.subjectblended-wing-bodyen_US
dc.subjectcomputational fluid dynamicsen_US
dc.subjectIncompressibleen_US
dc.subjectAerodynamicsen_US
dc.title16.100 Aerodynamics, Fall 2002en_US
dc.title.alternativeAerodynamicsen_US


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