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Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model
dc.contributor.authorCebeci, Tunceren_US
dc.contributor.authorJang, Hong-Mingen_US
dc.date.accessioned2010-06-11T18:17:06Z
dc.date.available2010-06-11T18:17:06Z
dc.date.issued1990en_US
dc.identifier.citationCebeci, Tuncer; Jang, Hong-Ming (1990). "Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model" JOURNAL OF AIRCRAFT, vol.27 no.8 (673-678). <http://hdl.handle.net/2027.42/76445>en_US
dc.identifier.issn0021-8669en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76445
dc.format.extent737110 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleInteractive boundary-layer method for unsteady airfoil flows - Quasisteady modelen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumMichigan, University, Ann Arboren_US
dc.contributor.affiliationotherDouglas Aircraft Co., Long Beach, CAen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76445/1/AIAA-25340-880.pdf
dc.identifier.doi10.2514/3.25340en_US
dc.identifier.sourceJOURNAL OF AIRCRAFTen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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