Comparative performance of combined gas turbine systems under three different blade cooling schemes

Author:

Najjar Yousef S.H,Alghamdi Abdullah S,Al-Beirutty Mohammad H

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference13 articles.

1. The advanced cooling technology for the 1500 °C class gas turbine: steam-cooled vanes and air-cooled blades;Nomoto;ASME Transactions, Journal for Gas Turbine and Power,1997

2. Design 60% net efficiency in frame 7/9 H steam-cooled CCGT;Farmer;Gas Turbine World,1995

3. A combined cycle designed to achieve greater than 60 percent efficiency;Briesch;ASME Transactions, Journal for Gas Turbine and Power,1995

4. 'Development requirements for an advanced gas turbine system;Bannister;ASME Transactions, Journal for Gas Turbine and Power,1995

5. Final report of the key technology development program for a next-generation high temperature gas turbine;Sato;ASME Transactions Journal for Gas Turbine and Power,1997

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1. Numerical Study on Cooling Performance of a Steam-Cooled Blade Based on Response Surface Method;Applied Sciences;2023-05-30

2. CFD Based Study of Gas Turbine Blade Cooling;Lecture Notes in Mechanical Engineering;2023

3. Heat transfer performance of steam/air flow in inverted V-shaped rib-roughened channels;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2021-05-18

4. Comprehensive Review on Leading Edge Turbine Blade Cooling Technologies;International Journal of Heat and Technology;2021-04-30

5. On the heat transfer characteristics of a Lamilloy cooling structure with curvatures with different pin fins configurations;International Journal of Numerical Methods for Heat & Fluid Flow;2020-09-22

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