3BUNKER R S.Gas Turbine Heat Transfer:10 Remaining Hot Gas Path Challenges Cooling[C]//Proceedings of ASME Turbo Expo.Barcelona,Spain:ASME IGTI,2006:90002. 被引量:1
4TOSHISHIGE A,ARIMURA H,KOENENKE C,et al.Development of an Air Cooled G Class Gas Turbine (the M501GAC)[C]//Proceedings of ASME Turbo Expo.Orlando,FL USA:ASME IGTI,2009:60321. 被引量:1
5BUNKER R S.Turbine Heat Transfer and Cooling:an Overview[C]//Proceedings of ASME Turbo Expo.San Antonio,Texas,USA:ASME IGTI,2013:94174. 被引量:1
6HANJ C,DUTTA S,EKKAD S.Gas Turbine Heat Transfer and Cooling Technology[M].2nd ed.New York:Taylor & Francis Press,2000. 被引量:1
7BOHN D,FUNKE H,HEUER T,BUTIKOFER J.Numerical and Experimental Investigations of the Influence of Different Swirl Ratios on the Temperature Streak Development in a 4-Stage Turbine[C]//Proceedings of ASME Turbo Expo.Munich Germany:ASME IGTI,2000:250. 被引量:1
8BARRINGER M D,THOLE K A,POLANKA M D.Effects of Combustor Exit Profiles on Vane Aerodynamic Loading and Heat Transfer in a High Pressure Turbine[J].ASME Journal of Turbomachinery,2009,131 (2):1-10. 被引量:1
9QURESHI I,BERETTA A,POVEY T.Effect of Simulated Combustor Temperature Non-Uniformity on HP Vane and End Wall Heat Transfer:an Experimental and Computational Investigation[J].Proc.IMechE,Part G:Journal of Aerospace Engineering,2011,222(G6):705-720. 被引量:1
10ONG J,MILLER R J.Hot Streak and Vane Coolant Migration in a Downstream Rotor[C]//Proceedings of ASME Turbo Expo.Berlin Germany:ASME IGTI,2008:43161. 被引量:1