Note on the influence of spanwise flow on lift distribution

dc.contributor.author	W. P. Jones	en_US
dc.date.accessioned	2014-10-21T15:52:07Z
dc.date.available	2014-10-21T15:52:07Z
dc.date.issued	1946	en_US
dc.identifier.other	ARC/R&M-2181	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3177
dc.description.abstract	The influence of spanwise flow on the lift distribution for a thin flexible wing of any plan form is considered. By the use of Eulel's equations for incompressible, inviscid flow, it is shown that the lift distribution is not appreciably affected provided the displacements of the wing are small.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Note on the influence of spanwise flow on lift distribution	en_US