The two-dimensional subsonic flow of an inviscid fluid about an aerofoil of arbitrary shape. Parts I to IV

dc.contributor.author	L. C. Woods	en_US
dc.date.accessioned	2014-10-21T15:53:00Z
dc.date.available	2014-10-21T15:53:00Z
dc.date.issued	1950	en_US
dc.identifier.other	ARC/R&M-2811	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3364
dc.description.abstract	The paper describes and applies exact methods of calculating the incompressible flow about thick aerofoils of general shape in a free stream, and about symmetrical aerofoils between channel walls. One of these methods is extended to an approximate treatment of subsonic compressible flow by making use of yon Karman's transformation.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The two-dimensional subsonic flow of an inviscid fluid about an aerofoil of arbitrary shape. Parts I to IV	en_US