Open AccessCalculation of Convective Heat Transfer in Square-Sectioned Gas Turbine Blade Cooling Channels
Author(s) -
Arash Saidi,
Bengt Sundén
Publication year - 1998
Language(s) - English
Resource type - Conference proceedings
DOI - 10.1115/98-gt-204
Subject(s) - mechanics , heat transfer , turbulence , turbine blade , convective heat transfer , rotation (mathematics) , churchill–bernstein equation , coupling (piping) , materials science , unstructured grid , turbine , computational fluid dynamics , thermodynamics , mechanical engineering , reynolds number , physics , mathematics , engineering , nusselt number , geometry
Internal cooling channels are commonly used to reduce the thermal loads on the gas turbine blades to improve overall efficiency. In this study a numerical investigation has been carried out to provide a validated and consistent method to deal with the prediction of the fluid flow and the heat transfer of such channels with square cross sections. The rotation modified Navier-Stokes and energy equations together with a low-Re number version of the k-ε turbulence model are solved with appropriate boundary conditions. The solution procedure is based on a numerical method using a collocated grid, and the pressure-velocity coupling is handled by the SIMPLEC algorithm. The computations are performed with the assumption of fully developed periodic conditions. The calculations are carried out for smooth ducts with and without rotation and effects of rotation on the heat transfer are described. Similar numerical calculations have carried out for channels with rib-roughened walls. The obtained results are compared with available experimental data and empirical correlations for the heat transfer rate and the friction factor. Some details of the flow and heat transfer fields are also presented.