Boundary-Layer Prediction Methods Applied to Cooling Problems in the Gas Turbine

dc.contributor.author	F. J. Bayley	en_US
dc.contributor.author	W. D. Morris	en_US
dc.contributor.author	J. M .Owen	en_US
dc.contributor.author	A. B. Turner	en_US
dc.date.accessioned	2014-10-20T11:06:07Z
dc.date.available	2014-10-20T11:06:07Z
dc.date.issued	1971	en_US
dc.identifier.other	ARC/CP-1164	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1177
dc.description.abstract	In this paper data obtained in a range of experimental investigations of cooling problems in the gas turbine are compared with theoretical predictions made by using a number of hypotheses concerning the analysis of turbulent boundary layers. Integral and differential theories have been used, and applied to flows over convection- and transpiration-cooled turbine blades and simplified representations of combustion systems and turbine discs. *Replaces A.R.C.32 050	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Boundary-Layer Prediction Methods Applied to Cooling Problems in the Gas Turbine	en_US