Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed

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dc.creator Bryce, W. W.
dc.date 2013-07-19T11:36:10Z
dc.date 2013-07-19T11:36:10Z
dc.date 1956-11
dc.date.accessioned 2022-05-09T10:17:24Z
dc.date.available 2022-05-09T10:17:24Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/7988
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4785
dc.description A radial parabolic induced velocity distribution agreeing closely with flight measurements has been used for the hovering case. Continues...
dc.language en
dc.publisher College of Aeronautics, Cranfield
dc.relation College Report
dc.relation 110
dc.title Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed
dc.type Report


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