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LES based aerothermal modeling of turbine blade cooling systems

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Academic year: 2021

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Table 2.1: Four main turbine blade failures and their temperature dependency [60].
Figure 2.4: Cooling flow in a turbine blade. Internal serpentine channels are visible by transparency.
Table 2.2: Advantages and drawbacks of the common blade internal cooling systems
Figure 2.6: Comparison of relative performance of different internal cooling systems.
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