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Heat transfer enhancement in combined cooling of the turbine blade leading edge
Authors:A. V. Shchukin  A. V. Il’inkov  S. G. Dezider’ev  S. N. Ivanov
Affiliation:1. Tupolev Kazan National Research Technical University, Kazan, Russia
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.
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