Hole Configuration Cooling Techniques for Gas Turbines Blades

Jaishri Dubey, Rajni Dewngan, Jaishri Patel, Prakash Kumar Sen, Shailendra Kumar Bohidar

Abstract


This paper is focused on internal cooling of blades and vanes on gas turbine. In this paper a hole configuration technique is used to predict the metal temperature of a gas turbine vane.

Keywords


Gas turbine; Hole configuration; Cooling film

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Copyright (c) 2014 Jaishri Dubey, Rajni Dewngan, Jaishri Patel, Prakash Kumar Sen, Shailendra Kumar Bohidar

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