from Aerothon.ACAirfoil import ACAirfoil
import pylab as pyl
Airfoils = ["S1223", "S1223_TC", "E423"] #Main wing
# Airfoils = ["NACA6413","E169", "NACA0015"]
#Airfoils = ["E220", "E221", "E222"]#Horz tail
#Airfoils = ["NACA0010","NACA0012","NACA0015"]#vert tail
#
for AirfoilName in Airfoils:
Airfoil = ACAirfoil(AirfoilName)
Airfoil.PlotReportPolars(fig=1, Re=500000) #main wing
# Airfoil.PlotReportPolars(fig=1, Re=200000)#tail horz and vert
pyl.subplot(311)
pyl.legend(Airfoils, loc="best")
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import pylab as pyl
Airfoils = ["E423","E423_B","S1223"]#Main wing
#Airfoils = ["NACA2408","E169"]#Horz tail
#Airfoils = ["NACA0010","NACA0012","NACA0015"]#vert tail
for AirfoilName in Airfoils:
Airfoil = ACAirfoil(AirfoilName)
Airfoil.PlotReportPolars(fig=1, Re=413946)#main wing
#Airfoil.PlotReportPolars(fig=1, Re=174000)#tail horz and vert
pyl.subplot(311)
pyl.legend(Airfoils, loc = "best")
pyl.show()
