OpenFoam, SALOME, all free tools for engineers
TSAGI HERITAGE, NACA23012, M=0.642, alpha = 1.67 grad
Posted May 20, 2014 at 04:11 by skeptik
Code:
#NACA 23012 exp. results alpha = 1°40' M=0.64 # Cp=(Pfoil - Pinfinity)/q; q = rho*U^2/2 #columns # x Cp #Upper 1 0.400 2.5 -0.380 5 -0.780 7.5 -1.000 10 -1.160 15 -1.300 20 -0.925 25 -0.750 30 -0.640 35 -0.580 40 -0.520 45 -0.455 50 -0.395 55 -0.340 60 -0.280 65 -0.220 70 -0.165 75 -0.115 80 -0.065 85 -0.010 90 0.055 95 0.120 100 0.210 #Lower 1 0.100 2.5 -0.120 5 -0.110 7.5 -0.070 10 -0.065 15 -0.145 20 -0.205 25 -0.235 30 -0.255 35 -0.255 40 -0.230 45 -0.195 50 -0.175 55 -0.170 60 -0.145 65 -0.110 70 -0.085 75 -0.060 80 -0.035 85 0.010 90 0.050 95 0.120 100 0.210
Total Comments 0