Abstract This paper reports the results of an experimental study of heat transfer using a model of the internal cooled surface of the turbine blade leading edge. We investigated a joint action of air jets and hemispherical protrusions on heat transfer from the concave surface of the leading edge model to air.
Heat transfer enhancement in combined cooling of the turbine blade leading edge
Russian Aeronautics (Iz VUZ) ; 56 , 4 ; 384-389
2013-10-01
6 pages
Article (Journal)
Electronic Resource
English
Heat transfer enhancement in combined cooling of the turbine blade leading edge
Online Contents | 2013
|Influence of Film Cooling Unsteadiness on Turbine Blade Leading Edge Heat Flux
Online Contents | 2012
|Heat Transfer Enhancement in Turbine Blade Internal Cooling Ducts
British Library Conference Proceedings | 2014
|Influence of Blade Leading Edge Geometry on Turbine Endwall Heat (Mass) Transfer
Online Contents | 2006
|