Heat Transfer and Friction Studies in a Tilted and Rib-Roughened Trailing-Edge Cooling Cavity with and without the Trailing-Edge Cooling Holes

<div>Measured Nusselt number variation with the local Reynolds number on all areas on the convex wall for the two rib geometries, open trailing-edge holes, and 1/2 blocked channel exit.</div>

International Journal of Rotating Machinery

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Figure 17

Figure 17: Heat Transfer and Friction Studies in a Tilted and Rib-Roughened Trailing-Edge Cooling Cavity with and without the Trailing-Edge Cooling Holes 

Figure 17 | Heat Transfer and Friction Studies in a Tilted and Rib-Roughened Trailing-Edge Cooling Cavity with and without the Trailing-Edge Cooling Holes 