Low-speed measurements of skin friction on a large half-model slender wing

dc.contributor.author	L. A. Wyatt	en_US
dc.contributor.author	L. F. East	en_US
dc.date.accessioned	2014-10-20T11:05:05Z
dc.date.available	2014-10-20T11:05:05Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/CP-1007	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1020
dc.description.abstract	Skin-friction measurements have been made on a half-model slender wing of 24 ft root chord at low subsonic speeds. The maximum root-chord Reynolds number was 30 x 10power6. The measurements were made using surface pitot-tubes formed by magnetically attaching razor-blade segments to the model surface. The results show that high levels of skin friction are present beneath the leading-edge vortex and are correlated satisfactorily with previous results obtained at lower Reynolds numbers.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Low-speed measurements of skin friction on a large half-model slender wing	en_US