Calculated Lift Distributions in Incompressible Flow on Some Sweptback Wings

dc.contributor.author	J.A Bagley	en_US
dc.contributor.author	G.M. Joyce	en_US
dc.date.accessioned	2014-10-20T11:03:41Z
dc.date.available	2014-10-20T11:03:41Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/CP-675	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/688
dc.description.abstract	In the course of a larger survey of some aerodynamic characteristics of a family of sweptback wings, the ion-speed lift distributions were calculated. The 35 planforms considered cover a range of leading-edge sweep angles from 55° to 70°, and aspect ratios from 2 to 3.9. The results are given here, together with a comparison with other calculations and with experimental results on one particular wing.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Calculated Lift Distributions in Incompressible Flow on Some Sweptback Wings	en_US