dc.contributor.author |
T. J. Hargest |
en_US |
dc.date.accessioned |
2014-10-21T15:52:45Z |
|
dc.date.available |
2014-10-21T15:52:45Z |
|
dc.date.issued |
1950 |
en_US |
dc.identifier.other |
ARC/R&M-2765 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3316 |
|
dc.description.abstract |
By means of Relf's analogy between aerodynamic streamline flow and electric potential flow, the theoretical pressure distributions around a series of conventional turbine blades in cascade have been determined over a range of incidence covered in some previously reported aerodynamic tests. The theoretical pressure distributions and their variation with incidence provide the basis of an explanation of the observed aerodynamic performance. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
The theoretical pressure distributions around some conventional |
en_US |