A lifting surface theory method for treating swept or slender wings in attached subsonic flow

dc.contributor.author	W. Kellaway	en_US
dc.date.accessioned	2014-10-21T15:50:58Z
dc.date.available	2014-10-21T15:50:58Z
dc.date.issued	1973	en_US
dc.identifier.other	ARC/R&M-3760	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3039
dc.description.abstract	A lifting surface theory method is described, capable of calculating the loading distribution on swept or slender planforms in attached, subsonic flow. Preliminary numerical results are presented which demonstrate that the method produces accurate, convergent loading solutions.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A lifting surface theory method for treating swept or slender wings in attached subsonic flow	en_US