dc.contributor.author |
P. R. Guyett |
en_US |
dc.contributor.author |
J. K. Curran |
en_US |
dc.date.accessioned |
2014-10-21T15:54:58Z |
|
dc.date.available |
2014-10-21T15:54:58Z |
|
dc.date.issued |
1958 |
en_US |
dc.identifier.other |
ARC/R&M-3171 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3740 |
|
dc.description.abstract |
A complete set of oscillatory aerodynamic stiffness and damping derivatives has been determined for a rectangular wing for rigid-wing modes of normal translation, pitch, and roll, in the range of frequency parameter 0.4 to 1.3, at low subsonic wind speeds. Each available comparison shows that the results are in satisfactory agreement with theoretical derivatives calculated by W. P. Jones and by Lawrence and Gerber. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Aerodynamic derivative measurements on a rectangular wing of aspect ratio 3.3 |
en_US |