International Journal of Rotating Machinery / 2015 / Article / Tab 2

Research Article

Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap

Table 2

Comparison of predicted by - RNG and SA models at Re = .

RNGSAExpt.% difference between
RNG and Expt.SA and Expt.RNG and SA

0.02500.02120.02336.8−9.915.2
0.03470.02640.019942.724.623.9
0.05100.03480.024552.029.631.8
12°0.07660.04960.033156.833.335.2