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 |