Measurements of the moments of inertia of the Morane-Saulnier M.S.760 'PARIS' aircraft

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dc.contributor.authorBradley, W. G.
dc.date.accessioned2017-07-06T11:23:46Z
dc.date.available2017-07-06T11:23:46Z
dc.date.issued1963-11
dc.description.abstractThis note describes the measurement of the moments of inertia, of a Morane-Saulnier M.S.760 'PARIS' aircraft. The moments of inertia in pitch, roll, and yaw were measured by the spring-constrained oscillation method. The cross-product of inertia and the inclination of the principal axis, were also determined by a variation of this method. Inertias were measured in three different fuel conditions. The results are given in Tables I - VI.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12168
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N/AERO-160en_UK
dc.relation.ispartofseries160en_UK
dc.titleMeasurements of the moments of inertia of the Morane-Saulnier M.S.760 'PARIS' aircraften_UK
dc.typeReporten_UK

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CoA. Aero Notes (1963-1975)