A digital computer program for the subsonic flow past turbomachine blades using a matrix method

dc.contributor.author	W. J. Calvert	en_US
dc.contributor.author	D. J. L. Smith	en_US
dc.date.accessioned	2014-10-21T15:51:40Z
dc.date.available	2014-10-21T15:51:40Z
dc.date.issued	1976	en_US
dc.identifier.other	ARC/R&M-3838	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3123
dc.description.abstract	A detailed description is given of a computer program for analysing the inviscid, subsonic compressible pressure distributions around the blades of axial, radial and mixed-flow turbomachines. The flow equations are combined to form a governing, Poisson-type differential equation for the stream function and the numerical solution is obtained by a finite difference matrix method. Solutions for several turbomachines, giving flow patterns and velocity distributions are included.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A digital computer program for the subsonic flow past turbomachine blades using a matrix method	en_US