Cooled MarkII blade surface pressure and temperature distribution by a conjugate heat transfer analysis using Reynolds stress baseline turbulence model

The paper discusses a conjugate heat transfer analysis of the MarkII blade, focusing on pressure and temperature distribution using the (RSM-BSL) turbulence model. The study involves numerical simulations and experimental validation, with a focus on cooling channels and turbulence modeling.

Published in Mechanical Engineering

Cooled MarkII blade surface pressure and temperature distribution by a conjugate heat transfer analysis using Reynolds stress baseline turbulence model
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  1. Conjugate Heat Transfer (CHT) Analysis: The paper highlights the importance of CHT in analyzing the thermal and pressure distribution on turbine blades. This could be a topic of interest for researchers and engineers working on gas turbine efficiency and cooling systems.

  2. Turbulence Models: The study compares different turbulence models, including the RSM-BSL model, which showed the best agreement with experimental results. This could spark a discussion on the effectiveness of various turbulence models in CFD simulations.

  3. Cooling Channel Design: The paper discusses the impact of cooling channel configuration on blade temperature distribution. This could be relevant for discussions on optimizing cooling systems in turbine blades.

  4. Experimental Validation: The study includes experimental validation of the cooling mass flow rate distribution, which could be a point of discussion for those interested in the practical application of numerical simulations.

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