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dc.contributor.author |
T. Niblett |
en_US |
dc.date.accessioned |
2014-10-20T11:05:29Z |
|
dc.date.available |
2014-10-20T11:05:29Z |
|
dc.date.issued |
1968 |
en_US |
dc.identifier.other |
ARC/CP-1046 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1059 |
|
dc.description.abstract |
Details are given of some of the methods of solving the flutter equations which have been programmed in Mercury Autocode at the R.A.E. Included is a method of following the variation of critical speed with a linear variation of the structural inertia, damping or stiffness. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
Methods of solving the flutter equations in use at R.A.E |
en_US |
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