An investigation at transonic speeds of the performance of various distributed rougness bands used to cause boundary-layer transition near the leading edge of a cropped delta half-wing

dc.contributor.author	E.W.E. Rogers et al	en_US
dc.date.accessioned	2014-10-20T11:02:33Z
dc.date.available	2014-10-20T11:02:33Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/CP-481	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/494
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	An investigation at transonic speeds of the performance of various distributed rougness bands used to cause boundary-layer transition near the leading edge of a cropped delta half-wing	en_US