The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section

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dc.contributor.author Nonweiler, T.
dc.date.accessioned 2012-09-11T14:58:04Z
dc.date.available 2012-09-11T14:58:04Z
dc.date.issued 1953-10
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/7564
dc.description.abstract An expression is deduced for the wave drag of a fully tapered swept wing of arbitrary section in the convenient form of a double integral involving the variation of wing-surface slope. It is concluded, in the general case, that the drag may best be computed by numerical integration, the method for which will be the subject of a further report. Continues … en_UK
dc.language.iso en en_UK
dc.publisher College of Aeronautics, Cranfield en_UK
dc.relation.ispartofseries College Reports en_UK
dc.relation.ispartofseries 76 en_UK
dc.title The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section en_UK
dc.type Report en_UK


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