A subsonic lifting-surface theory for low-aspect-ratio wings

dc.contributor.author	C. R. Taylor	en_US
dc.date.accessioned	2014-10-21T15:54:19Z
dc.date.available	2014-10-21T15:54:19Z
dc.date.issued	1956	en_US
dc.identifier.other	ARC/R&M-3051	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3620
dc.description.abstract	A method is developed for determining the loading on low-aspect-ratio wings. By allowing for down stream effects on the flow at a station on the wing and for the trailing-edge condition, the method improves on R. T. Jones's theory for wings of very small aspect ratio. Calculations have been made for thirteen different wings and a comparison with other methods of solution is given for some cases.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A subsonic lifting-surface theory for low-aspect-ratio wings	en_US