In order to enhance the cooling performance of turbine blades, novel cooling
channels filled with X-shaped truss array were investigated in this study.
The flow mechanism and heat transfer characteristic of the cooling channel
filled with X-shaped truss array were analyzed numerically. The empirical
correlations of friction coefficient and Nusselt number related to the inlet
Reynolds number (10,000 to 60,000) and truss rod inclination angle (30? to
45?) were fitted. The results show that the secondary flow vortex in the
channel and the Nusselt number on the channel wall both show periodic
distributions along the streamwise direction. The row-averaged Nusselt
number and friction coefficient of the channel first decrease quickly and
then decrease slowly along the streamwise direction. When truss rod
inclination angle increases from 30? to 60?, the whole-averaged Nusselt
number and the whole friction coefficient of the channel increase by 25.4%
to 52.3% and 1.19 to 1.33 times respectively under different Reynolds
number. The channel with truss rod inclination angle of 45? has the best
comprehensive thermal performance. In all cases, the ratio of heat transfer
quantity of the truss rod surface to the total heat transfer quantity of the
channel ranges from 22.9% to 42.3%. The increase of Reynolds number improves
the heat transfer quantity of the channel wall and the increase of truss rod
inclination angle reduces the heat transfer quantity of the channel wall.