An approximate method for calculating the laminar boundary layer on an infinite swept wing with arbitrary velocity and suction distributions

dc.contributor.author	A. W. Lindfield	en_US
dc.contributor.author	H. G. Pinsent	en_US
dc.date.accessioned	2014-10-20T11:02:39Z
dc.date.available	2014-10-20T11:02:39Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/CP-516	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/529
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	An approximate method for calculating the laminar boundary layer on an infinite swept wing with arbitrary velocity and suction distributions	en_US