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 |