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

Nonweiler, T.

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