Tests in the compressed air tunnel on two aerofoil sections having a large scale effect on CLmax at a critical reynolds number

dc.contributor.author	C. Salter	en_US
dc.contributor.author	H. M. Lee	en_US
dc.contributor.author	R. C. Owen	en_US
dc.date.accessioned	2014-10-20T11:00:06Z
dc.date.available	2014-10-20T11:00:06Z
dc.date.issued	1952	en_US
dc.identifier.other	ARC/CP-92	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/105
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Tests in the compressed air tunnel on two aerofoil sections having a large scale effect on CLmax at a critical reynolds number	en_US