Some actuator-disc theories for the flow of air through an axial turbo-machine

dc.contributor.author	J. H. Horlock	en_US
dc.date.accessioned	2014-10-21T15:54:15Z
dc.date.available	2014-10-21T15:54:15Z
dc.date.issued	1952	en_US
dc.identifier.other	ARC/R&M-3030	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3597
dc.description.abstract	Using actuator-disc theory, simplified methods are given for the solution of the direct problem of the incompressible flow of air through an axial-flow turbo-machine. Calculations based on these methods are compared with other approximate solutions to the flow through a model compressor stage.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Some actuator-disc theories for the flow of air through an axial turbo-machine	en_US