An exact test case for the plane potential flow about two adjacent lifting aerofoils

dc.contributor.author	B. R. Williams	en_US
dc.date.accessioned	2014-10-21T15:50:47Z
dc.date.available	2014-10-21T15:50:47Z
dc.date.issued	1971	en_US
dc.identifier.other	ARC/R&M-3717	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2993
dc.description.abstract	A method for calculating the incompressible potential flow about two particular aerofoil sections is presented. The potential flow about two lifting circles is calculated by the method of images, and the two circles are mapped conformally on to two aerofoils by a double application of the Karman-Trefftz transformation. The results for the test cases are then compared with those from a numerical method, which uses a surface distribution of sources.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	An exact test case for the plane potential flow about two adjacent lifting aerofoils	en_US