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Minimization of the Number of Cooling Holes in Internally Cooled Turbine Blades
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G.S. Dulikravich,
Published/Copyright:
December 1, 1992
Published Online: 1992-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Experimental Determination of Prewhirl Effects on Centrifugal Compressor Internal Aerodynamics
- Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring
- Minimization of the Number of Cooling Holes in Internally Cooled Turbine Blades
- A Computational Study of Gas Turbine Combustion Chamber Flow Field
- Effects of Length and Configuration of Transverse Discrete Ribs on Heat Transfer and Friction for Turbulent Flow in a Square Channel
- Gas Turbine Axial Compressor Fouling: A Unified Treatment of its Effects, Detection, and Control
Articles in the same Issue
- CONTENTS
- Experimental Determination of Prewhirl Effects on Centrifugal Compressor Internal Aerodynamics
- Preliminary Development of an Intelligent Computer Assistant for Engine Monitoring
- Minimization of the Number of Cooling Holes in Internally Cooled Turbine Blades
- A Computational Study of Gas Turbine Combustion Chamber Flow Field
- Effects of Length and Configuration of Transverse Discrete Ribs on Heat Transfer and Friction for Turbulent Flow in a Square Channel
- Gas Turbine Axial Compressor Fouling: A Unified Treatment of its Effects, Detection, and Control
