Low-speed wind-tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio

dc.contributor.author	D. H. Peckham	en_US
dc.date.accessioned	2014-10-20T11:05:34Z
dc.date.available	2014-10-20T11:05:34Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1076	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1089
dc.description.abstract	Results are given of six-component balance measurements on a gothic wing of unit aspect ratio fitted either with a pair of fins, at various spanwise locations, or a single central fin. Each fin was triangular in shape, with a leading-edge sweep of 60 degrees and an area 12.5% of chat of the wing.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Low-speed wind-tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio	en_US