The rolling power of an elastic swept wing

dc.contributor.author	E. G. Broadbent	en_US
dc.date.accessioned	2014-10-21T15:53:16Z
dc.date.available	2014-10-21T15:53:16Z
dc.date.issued	1950	en_US
dc.identifier.other	ARC/R&M-2857	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3413
dc.description.abstract	An iterative method of solution is given for the problem of loss in rolling power due to wing deformation. The method is applicable at subsonic or supersonic speeds, and compressibility effects are allowed for, provided the variation of the aerodynamic derivatives with Mach number is known. The numerical labour involved in the solution is not great and the accuracy is considerably greater than can be achieved by the semi-rigid method.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The rolling power of an elastic swept wing	en_US