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 |
|