The determination in flight of the body drag and the mean blade profile drag coefficient of a helicopter

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dc.creator Bartholomew, F. E.
dc.creator Marshall, W. S. D.
dc.date 2012-07-26T12:49:00Z
dc.date 2012-07-26T12:49:00Z
dc.date 1952-04
dc.date.accessioned 2022-05-09T10:17:19Z
dc.date.available 2022-05-09T10:17:19Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/7431
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4731
dc.description Slight modifications have been made to the energy equation which enables the results of partial climb tests to be plotted as two straight lines, the slopes of which are measures of the body drag of the helicopter and the mean profile drag coefficient of the rotor blades. Sufficient data has been analysed to show that the method can be used to obtain an accurate measurement of the body drag. Continues …
dc.language en
dc.publisher College of Aeronautics, Cranfield
dc.relation College Report
dc.relation 56
dc.title The determination in flight of the body drag and the mean blade profile drag coefficient of a helicopter
dc.type Report


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