The theoretical pressure distributions around some conventional

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