[anon_k]

Hi,

I went to download SU2_EDU today, to install on a new computer. The parallel windows binary link is broken. Also, I noticed this awhile ago, but the python script you have to make the pressure plot is broke. I hacked a fix awhile back, but you may want to provide a functioning version in the download. The hack I did is as follows:

import os, time
import pandas as pd
from optparse import OptionParser
from numpy import *
from matplotlib import pyplot as plt
from matplotlib import mlab

filename = "surface_flow.csv"

# Load the csv file with the airfoil coordinate and pressure data (sorted)

data = pd.read_csv(filename)
data = data.sort('Global_Index')
data.to_csv(filename, index=False)
data = mlab.csv2rec(filename, comments='#', skiprows=0, checkrows=0)

# Plot the airfoil shape and pressure distribution

fig = plt.figure()
ax1 = fig.add_subplot(111)
ax1.plot(data.x_coord[:],data.pressure_coefficient[:],'-b',linewidth = 2.0)
ax1.set_ylim(ax1.get_ylim()[::-1])
ax1.set_xlabel(r'$x/c$', fontsize=20)
ax1.set_ylabel(r'$C_p$', fontsize=20)

ax2 = ax1.twinx()
ax2.plot(data.x_coord[:],data.y_coord[:],'-k',linewidth = 1.5)
ax2.axis('equal')
ax2.axis('off')
ax2.set_xlim([-0.02,1.02])
ax2.set_ylim([-0.1,0.7])
ax2.set_ylabel(r'$y / c$', fontsize=20)
plt.savefig('pressure_distribution.png',format='pn g')