def run_test_aero_analysis():
timer = Timer()
af = cst_x(np.array([0.18723832, 0.2479892, 0.26252777, 0.31606257, 0.0819584, -0.11217863, -0.14363534, -0.06480575, -0.27817776, -0.08874038]))
af._analyze_geometry()
af.display()
timer.lap('read db')
pol1 = af.get_jfoil_polar(0.2,3e6)
timer.lap('javafoil')
pol2 = af.get_xfoil_polar(0.2,3e6)
timer.stop('xfoil')
plt.figure(1)
plt.hold(True)
plt.grid(True)
plt.plot(pol1.alpha,pol1.cd)
plt.plot(pol2.alpha,pol2.cd)
plt.show()
def main():
yplus = np.array([0.25, 0.5, 1.0, 5.0, 10.0, 25.0])
gridScale = np.array([0.5, 0.75, 1.0, 2.0, 4.0, 6.0])
zTE = 0.005
Mach = 0.85
alt = 10000
alpha = 0.0
npts = 101
t = Timer()
fc = flight_conditions.FlightConditions(Mach, alt)
A = np.array([0.06421182,0.11882206,0.12335525,0.12384311,0.11381198,
-0.01503971,-0.07024083,-0.04311071,0.02437696])
#af = af_cfd_analysis.airfoil.cst_x(A, nPts=npts)
af = af_cfd_analysis.airfoil.Airfoil()
af.read_txt('N64A206.txt')
af.display()
#af.set_trailing_edge(zTE)
fid = open('grid_convergence.txt','wt')
fid.write('yplus\tgridSize\ttime\tcl\tcd\tcm\n')
fid.close()
nCase = 0
for i,yp in enumerate(yplus):
for j,gs in enumerate(gridScale):
t.start()
nCase += 1
cl, cd, cm, gridSize = run_analysis(af, fc, alpha, yp, gs,nCase)
duration = t.lap()
out = '%.1f\t%d\t%.4f\t%.6f\t%.6f\t%.6f\n'%(yp,gridSize,duration,cl,cd,cm)
fid = open('grid_convergence.txt','a')
fid.write(out)
fid.close()
print out
t.stop()