Preliminary Results of Low Speed Wind Tunnel Tests on a Gothic Wing of Aspect Ratio 1.0

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dc.contributor.author D. H. Peckham en_US
dc.contributor.author S. A. Atkinson en_US
dc.date.accessioned 2014-10-20T11:02:38Z
dc.date.available 2014-10-20T11:02:38Z
dc.date.issued 1960 en_US
dc.identifier.other ARC/CP-508 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/521
dc.description.abstract This note gives preliminary results of low speed balance measurements and flow visualisation tests, on a wing of aspect ratio 1.0. The wing had a convex parabolic leading-edge shape in plan view, and an unswept trailing edge - such wings are now termed "Gothic". All edges were sharp, the centre section was 12% biconvex, and transverse sections were diamond-shaped. Results of tests on a strictly comparable delta wing are not yet available, but where possible the results are compared with tests on other wings of aspect ratio 1.0 with unswept trailing edges. en_US
dc.relation.ispartofseries Aeronautical Research Council Current Papers en_US
dc.title Preliminary Results of Low Speed Wind Tunnel Tests on a Gothic Wing of Aspect Ratio 1.0 en_US


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