Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges

dc.contributor.author	D. H. Peckham	en_US
dc.date.accessioned	2014-10-21T15:55:02Z
dc.date.available	2014-10-21T15:55:02Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/R&M-3186	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3755
dc.description.abstract	A series of three thick uncambered slender wings and twelve flat-plate slender wings, all with sharp edges, have been tested in the 13 ft x 9 ft Low-Speed Wind Tunnel at the Royal Aircraft Establishment, Bedford. Pressure plotting, balance measurements and flow-visualisation tests were made to investigate the effects of plan-form shape, thickness, and aspect ratio on their aerodynamic characteristics at low speeds.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges	en_US