dc.contributor.author |
N. C. Lambourne et al |
en_US |
dc.date.accessioned |
2014-10-21T15:53:26Z |
|
dc.date.available |
2014-10-21T15:53:26Z |
|
dc.date.issued |
1952 |
en_US |
dc.identifier.other |
ARC/R&M-2895 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3454 |
|
dc.description.abstract |
Partly to gain experience of aero-elastic models constructed from Xylonite, and partly to provide information regarding loss of rolling power due to wing distortion, a tip-to-tip model of the wings of a Spitfire aircraft was constructed. It was mounted on a longitudinal axis in a wind tunnel so that it could roll continuously. Rates of rolling were measured for a range of air speeds and the results are compared with those of calculations. The variation of rolling power with air speed was calculated by : (a) the Collar and Broadbent method (R. & M. 2186) which is based on strip theory, (b) a method developed by H. C. Garner based on lifting-line theory. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Rolling power measurements and comparative calculations for a flexible model wing constructed from xylonite |
en_US |