Natural frequencies and modes of a model delta aircraft

dc.contributor.author	D. R. Gaukroger	en_US
dc.date.accessioned	2014-10-21T15:52:44Z
dc.date.available	2014-10-21T15:52:44Z
dc.date.issued	1950	en_US
dc.identifier.other	ARC/R&M-2762	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3313
dc.description.abstract	Resonance tests on a model delta wing are described. Consideration is given to the effect of inertia distribution on the first three normal symmetric modes of vibration. The mean centre of gravity position, fuselage pitching moment of inertia and wing inertia axis have been independently varied, and the effect of concentrated tip masses has been examined. Results are given which are intended as a general guide in flutter calculations.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Natural frequencies and modes of a model delta aircraft	en_US