A technique for analysing the results of a flutter calculation

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dc.contributor.author J. C. A. Baldock en_US
dc.date.accessioned 2014-10-21T15:51:00Z
dc.date.available 2014-10-21T15:51:00Z
dc.date.issued 1973 en_US
dc.identifier.other ARC/R&M-3765 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3045
dc.description.abstract A technique is presented for condensing a multi-degree-of-freedom flutter calculation so that similar flutter conditions are achieved with two degrees-of-freedom. Use is made of digital computer programmes, and the process is largely automatic. Examples of the application of the technique are given, and show that systems can often be reduced to two normal modes, or to two orthogonal combinations of normal modes, and that these modes can be interpreted physically. A detailed analysis of one of the derived two degree-of-freedom systems is made. This analysis uses a method restricted to a binary system, and so the condensation technique made possible the application of this method. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title A technique for analysing the results of a flutter calculation en_US


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