International Journal of Rotating Machinery / 2015 / Article / Tab 1

Research Article

Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap

Table 1

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

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

0.5420.5380.40625.124.50.7
0.9900.9970.86812.312.9−0.7
1.4051.4351.2858.510.5−2.1
12°1.7561.8271.6466.39.9−4.0