August 17, 2025Open Access

Cooling Performance Prediction of Turbine Blades and Vanes for Conceptual Design

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A new method calculates cooling performance in turbine blades and vanes, enhancing design efficiency.
The approach shows a potential 32% reduction in cooling mass flow by optimizing cooling techniques and temperatures.
Assessment involves parametric studies on main gas and cooling air temperatures alongside material temperature.
Collaboration with MTU Aero Engines supports practical application in high-pressure turbine design.

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New method improves cooling performance assessment in turbine blades and vanes, suggesting innovative design techniques.

Bachmann et al. (2025) studied this question.

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