dc.contributor.author |
C. W. Skingle |
en_US |
dc.contributor.author |
D. R. Gaukroger |
en_US |
dc.contributor.author |
G. A. Taylor |
en_US |
dc.date.accessioned |
2014-10-20T11:05:33Z |
|
dc.date.available |
2014-10-20T11:05:33Z |
|
dc.date.issued |
1969 |
en_US |
dc.identifier.other |
ARC/CP-1070 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1083 |
|
dc.description.abstract |
An experiment to excite the flapping modes of a two-blade nonarticulated model rotor is described. The experiment was designed to develop a method of exciting a blade whilst it is rotating, and to measure the change of natural frequencies due to centrifugal effects. Three of the first four modes of the blade were excited over a range of rotational speeds, and the variations of frequency and damping with rotational speed are given for each mode. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
A preliminary experiment in resonance testing a rotating blade |
en_US |