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

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dc.creator Bradley, W. G.
dc.date 2017-07-06T11:23:46Z
dc.date 2017-07-06T11:23:46Z
dc.date 1963-11
dc.date.accessioned 2020-11-30T18:29:56Z
dc.date.available 2020-11-30T18:29:56Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/12168
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/12168
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4138
dc.description.abstract This 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.
dc.language en
dc.publisher College of Aeronautics
dc.relation CoA/N/AERO-160
dc.relation 160
dc.title Measurements of the moments of inertia of the Morane-Saulnier M.S.760 'PARIS' aircraft
dc.type Report


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