Table 1.
Summary of the airfoil lift coefficient calibration case
Case
a
1
c
l
Experimental calibration data (Ladson, 1988)
–
1.0707
k
-
ω
SST, default coefficient
0.31
1.0847
k
-
ω
SST, turbo-RANS optimized
0.28
1.0706
Case
a
1
c
l
Experimental calibration data (
Ladson, 1988
)
–
1.0707
k
-
ω
SST, default coefficient
0.31
1.0847
k
-
ω
SST, turbo-RANS optimized
0.28
1.0706
Source:
Author’s own work
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