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This document presents a study on gas turbine combustor liner cooling calculation methods, highlighting the need for improved accuracy in cooling calculations due to reduced cooling air flow rates. It introduces a new method for calculating radiation from non-luminous gases and emphasizes that the combustor casing wall temperature cannot be assumed equal to the combustor inlet air temperature. The authors suggest a more precise approach to emissivity calculations, which is crucial for effective combustor de

Author

Yi Zhang

Language

EN