Numerical prediction of flow and heat transfer in the coolant passages of a gas turbine rotor blade /

Numerical prediction of three- dimensional flow and heat transfer was performed for four cases. 1) A rotating/non-rotating smooth square channel with 180⁰ bend in which the rotation number was varied from 0 to 0.24, the inlet coolant-to-wall density ratio was varied from 0 to 0.22, while the Reynold...

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