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Hot Streak Migration in a Turbine Stage: Integrated Design to Improve Aerothermal Performance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Hot streaks can cause localized hot spots on the blade surfaces in a high pressure turbine, increasing the heat load locally and even leading to material loss in regions such as the rotor ...
Integrated Combustor Turbine Design for Improved Aerothermal Performance: Effect of Dilution Air Control
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The effect of dilution air control in a combustor on the heat load distribution of an axial turbine with nonaxisymmetric endwall profiling is examined. Endwall profiling is a more common design ...
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