solver.py
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	import numpy as np
	import fenics as fen
	from airfoil_engine import AirfoilScatteringEngine

	verb = 0

	####################

	homog = True
	homog = False

	####################

	k0 = 5e2 * 2 * np.pi / 340
	kappa = 5e2 * 2 * np.pi / 340

	theta = np.pi * - 45 / 180.
	mesh = fen.Mesh('../data/mesh/airfoil2412_1.xml')

	solver = AirfoilScatteringEngine(kappa, theta, verbosity = verb,
	degree_threshold = 8)

	uinc = solver.liftDirichletData(k0)
	if homog:
	uhtot = solver.solve(kappa, homogeneized = homog)
	uh = uhtot + uinc
	else:
	uh = solver.solve(kappa, homogeneized = homog)
	uhtot = uh - uinc
	print(solver.norm(uh))
	print(solver.norm(uhtot))
	solver.plot(fen.project(solver.diffusivity[0], solver.V).vector(),
	what = 'Real', name = 'a')
	solver.plot(uinc, what = 'Real', name = 'u_inc')
	solver.plot(uh, what = 'ABS')
	solver.plot(uhtot, what = 'ABS', name = 'u + u_inc')
	solver.outParaviewTimeDomain(uh, omega = kappa, forceNewFile = False,
	filename = "out/out_{}_".format(kappa))
	solver.outParaviewTimeDomain(uhtot, omega = kappa, forceNewFile = False,
	filename = "out/outT_{}_".format(kappa))