Further tests on a three-stage turbine of low reaction to examine the effects of reduced rotor pitch and improved sealing

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dc.contributor.author I. H. Johnston en_US
dc.contributor.author D. C. Dransfield en_US
dc.date.accessioned 2014-10-20T11:04:27Z
dc.date.available 2014-10-20T11:04:27Z
dc.date.issued 1966 en_US
dc.identifier.other ARC/CP-861 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/874
dc.relation.ispartofseries Aeronautical Research Council Current Papers en_US
dc.title Further tests on a three-stage turbine of low reaction to examine the effects of reduced rotor pitch and improved sealing en_US


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