Some experiments with fluidic devices in aviation kerosene

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dc.creator Taylor, A. F.
dc.date 2017-07-31T08:48:13Z
dc.date 2017-07-31T08:48:13Z
dc.date 1969-04
dc.date.accessioned 2020-11-30T18:29:58Z
dc.date.available 2020-11-30T18:29:58Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/12250
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/12250
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4153
dc.description.abstract Comparatively little has been published on ‘heavy current’ fluidic devices yet their advantages suggest that they have a place in aircraft fluid systems. As a first brief step towards assessing their value to the aircraft fuel system designer several devices were tested, singly and in pairs; in aviation kerosene. Some of the results from these experiments are given and discussed and it is considered that further work could produce some extremely worthwhile information.
dc.language en
dc.publisher College of Aeronautics
dc.relation CoA/N/AERO-176
dc.relation 176
dc.title Some experiments with fluidic devices in aviation kerosene
dc.type Report


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