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.
