Research Article
Dusting Hole Film Cooling Heat Transfer on a Transonic Turbine Blade Tip
Figure 8
Locations A and B as well as regions for area averaging presented with respect to heat transfer coefficient ratio distribution, with film cooling. (a) Dataset 10, 0.8 mm tip gap, . (b) Dataset 4, 1.4 mm tip gap, .
(a) |
(b) |