Rotating Stall and Casing Wall Boundary Layers in an Axial Flow Compressor

dc.contributor.author	C. Lakhwani	en_US
dc.date.accessioned	2014-10-20T11:06:21Z
dc.date.available	2014-10-20T11:06:21Z
dc.date.issued	1973	en_US
dc.identifier.other	ARC/CP-1255	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1268
dc.description.abstract	An experimental investigation has been made to study the effect of casing wall boundary layers upon the rotating stall characteristics of an axial flow compressor in an isolated rotor row configuration. The boundary layer was modified by fixing circular rings of different wire diameters to the outer casing. A significant alteration of the rotating stall characteristics was obtained with regard to changes in flow coefficient at stall onset and cessation. *Replaces A.R.C.33 898	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Rotating Stall and Casing Wall Boundary Layers in an Axial Flow Compressor	en_US