An improved method for calculating generalised airforces on oscillating wings in subsonic flow

dc.contributor.author	G. Long	en_US
dc.date.accessioned	2014-10-21T15:50:34Z
dc.date.available	2014-10-21T15:50:34Z
dc.date.issued	1969	en_US
dc.identifier.other	ARC/R&M-3657	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2928
dc.description.abstract	A lifting-surface theory of Multhopp-type has been revised to include an improved method of spanwise integration and programmed in Fortran IV. Generalised airforces have been calculated for three wings and the effects of varying the number of collocation points and the accuracy of spanwise integration are discussed.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	An improved method for calculating generalised airforces on oscillating wings in subsonic flow	en_US