A method of calculating the velocity distribution on annular aerofoils in incompressible flow

dc.contributor.author	J. A. Bagley	en_US
dc.contributor.author	N. B. Kirby	en_US
dc.contributor.author	P. J. Marcer	en_US
dc.date.accessioned	2014-10-21T15:54:51Z
dc.date.available	2014-10-21T15:54:51Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/R&M-3146	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3714
dc.description.abstract	A method of calculating the velocity distribution in incompressible flow on annular aerofoils of moderate thickness/chord ratio and camber, and reasonably large radius/chord ratio (the order of 1 or greater), is developed, based on the use of distributions of singularities on a cylinder whose velocity fields are tabulated here. The annular wing at zero incidence is treated first, and then the wing at incidence. Examples of the calculated velocity distributions on various aerofoils are given.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A method of calculating the velocity distribution on annular aerofoils in incompressible flow	en_US