Skip to main content
. Author manuscript; available in PMC: 2019 Sep 18.
Published in final edited form as: J Turbomach. 2016 Sep;138(9):TURBO-15-1305. doi: 10.1115/1.4032839

TABLE 2.

TABLE OF PARAMETERS FOR NON-DIFFUSION TYPE HOLES (L/D=4, DR=1.05)

Hole Geometry Nominal Blowing Ratio Coolant Exit Temperature (°F) Freestream Recovery Temperature (°F) P/D Re Uncertainty in η (%) Uncertainty (°F)
Smooth Circular 1.0 54.0 73.4 6 11000 1.0 0.20
Smooth Circular 1.5 53.6 75.7 6 11000 0.9 0.20
Smooth Circular 2.0 53.1 75.9 6 11000 0.9 0.20
Smooth Circular 2.5 52.6 76.1 6 11000 0.9 0.20
Smooth Circular 2.0 53.4 75.9 3 7400 0.9 0.20
Smooth Compound Angle 1.0 50.3 71.8 6 11000 0.9 0.20
Smooth Compound Angle 1.5 48.1 72.0 6 11000 0.8 0.20
Smooth Compound Angle 2.0 48.0 72.4 6 11000 0.8 0.20
Smooth Compound Angle 2.5 50.1 74.4 6 11000 0.8 0.20
Smooth Compound Angle 2.0 47.9 72.3 3 7400 0.8 0.20
Spiral Same Direction 1.0 57.3 73.7 6 11000 0.3 0.05
Spiral Same Direction 1.5 52.6 72.3 6 11000 0.3 0.05
Spiral Same Direction 2.0 49.2 72.1 6 11000 0.2 0.05
Spiral Same Direction 2.5 45.3 72.0 6 11000 0.2 0.05
Spiral Alternating Direction 1.0 49.7 71.0 6 11000 0.2 0.05
Spiral Alternating Direction 1.5 47.3 71.5 6 11000 0.2 0.05
Spiral Alternating Direction 2.0 46.9 71.8 6 11000 0.2 0.05
Spiral Alternating Direction 2.5 46.9 71.9 6 11000 0.2 0.05
Spiral Alternating Direction 2.0 46.7 71.6 3 7400 0.2 0.05