Approximate two-dimensional aerofoil theory part 5 the positions of maximum velocity and theoretical CL-ranges

dc.contributor.author	S. Goldstein	en_US
dc.date.accessioned	2014-10-20T11:00:02Z
dc.date.available	2014-10-20T11:00:02Z
dc.date.issued	1952	en_US
dc.identifier.other	ARC/CP-72	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/85
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Approximate two-dimensional aerofoil theory part 5 the positions of maximum velocity and theoretical CL-ranges	en_US