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dc.contributor.advisorPlatzer, Max F.
dc.contributor.authorMathre, John Mark
dc.dateDecember 1988
dc.date.accessioned2012-11-27T18:06:23Z
dc.date.available2012-11-27T18:06:23Z
dc.date.issued1988-12
dc.identifier.urihttp://hdl.handle.net/10945/22965
dc.description.abstractCebeci's viscous/inviscid interaction program was applied to the analysis of steady, two dimensional, incompressible flow past four airfoils, the NACA 66₃-018, 0010 (Modified), 4412 and the Wortmann FX 63-137. Detailed comparisons with the available experimental results show that the essential features are correctly modelled, but that significant discrepancies are found in regions of flow separations.
dc.description.urihttp://archive.org/details/computationalinv1094522965
dc.format.extent143 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
dc.titleComputational investigation of incompressible airfoil flows at high angles of attacken_US
dc.typeThesisen_US
dc.contributor.secondreaderHoward, R.M.
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautics and Astronautics
dc.subject.authorcomputational analysis of inviscid
dc.subject.authorviscous and interaction schemes
dc.description.serviceLieutenant, United States Navy
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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