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 |