Wind-tunnel flutter tests on a model delta wing under fixed and free root conditions

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dc.contributor.author D. R. Gaukroger en_US
dc.contributor.author E. W. Chapple en_US
dc.contributor.author A. Milln en_US
dc.date.accessioned 2014-10-21T15:53:05Z
dc.date.available 2014-10-21T15:53:05Z
dc.date.issued 1950 en_US
dc.identifier.other ARC/R&M-2826 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3381
dc.description.abstract Wind-tunnel tests on a model wing of delta plan form are described. Tests have heen made with the wing root fixed and also with the root free in pitch and vertical translation. Critical flutter speed and frequency are given for a wide range of variation of wing and fuselage inertia parameters. The results show that, under root-free conditions, body freedom flutter occurs at low values of fuselage pitching moment of inertia, but that at higher values the flutter is similar to that obtained with root-fixed conditions. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Wind-tunnel flutter tests on a model delta wing under fixed and free root conditions en_US


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