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Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/19063
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dc.contributor.authorStandingford, David William Finen
dc.date.issued1997en
dc.identifier.urihttp://hdl.handle.net/2440/19063-
dc.descriptionBibliography: leaves 164-172.en
dc.descriptionxii, 172 leaves : ill. (some col.) ; 30 cm.en
dc.description.abstractThe task of calculating the aerodynamic load distribution on a thin three-dimensional lifting surface or wing of finite aspect ratio at small angle of attack presents difficulties for most numerical methods. The two-dimensional lifting-surface integral equation that must be solved is highly singular, and does not possess analytic solutions, even for simple plan-form geometries such as rectangles or ellipses.en
dc.format.extent82706 bytesen
dc.format.mimetypeapplication/pdfen
dc.language.isoenen
dc.subject.lcshNumerical analysis.en
dc.subject.lcshAerodynamic load.en
dc.titleOptimal lifting surfaces, including end plates, ground effect & thickness / David William Fin Standingford.en
dc.typeThesisen
dc.contributor.schoolDept. of Applied Mathematicsen
dc.provenanceThis electronic version is made publicly available by the University of Adelaide in accordance with its open access policy for student theses. Copyright in this thesis remains with the author. This thesis may incorporate third party material which has been used by the author pursuant to Fair Dealing exception. If you are the author of this thesis and do not wish it to be made publicly available, or if you are the owner of any included third party copyright material you wish to be removed from this electronic version, please complete the take down form located at: http://www.adelaide.edu.au/legals-
dc.description.dissertationThesis (Ph.D.)--University of Adelaide, Dept. of Applied Mathematics, 1998en
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