Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing part 1 three-dimensional tests on the wing part 2 two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section

dc.contributor.author	Joseph Black	en_US
dc.date.accessioned	2014-10-20T11:00:14Z
dc.date.available	2014-10-20T11:00:14Z
dc.date.issued	1953	en_US
dc.identifier.other	ARC/CP-137	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/150
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing part 1 three-dimensional tests on the wing part 2 two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section	en_US