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- W2200133021 abstract "Heat transfer enhancement problem of turbine blade cooling passage has been solved numerically in this paper. Basic fluid dynamics equations like mass, momentum and energy equations are solved to enhance turbulent heat transfer. Dimpled channel heat transfer problem is formulated considering three dimensionless design variables. The objective functions are pressure drop and Nusselt number. Dimple on the wall of flow passage increases turbulence and pressure drop. Combining these two objectives, the shape of the dimple channel has been optimized. D-optimal design generated design points are used to design the channels and flow field is solved by RANS analysis. The Nusselt number and pressure drop objective functions are combined using weighting factor method to make final single objective function. Surrogate models like response surface, Kriging, radial basis neural network and weighted average models are used for optimization. Evaluation of surrogate models as well as optimal design of the dimpled channel has been presented in this paper." @default.
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- W2200133021 date "2006-11-01" @default.
- W2200133021 modified "2023-09-24" @default.
- W2200133021 title "Heat Transfer Enhancement by Shape Optimization of Dimpled Channel" @default.
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