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ktreff_aerofoil.py
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import math
import matlab.engine
import numpy as np
import pandas as pd
from scipy.interpolate import griddata
class KarmanTrefftzAerofoil(object):
"""
Object to represent Karman-Trefftz aerofoil generated by MATLAB.
"""
def __init__(self, **kwargs):
self.alpha = float(kwargs['alpha']) * math.pi / 180.0 # Input in degrees, MATLAB requires radians
self.eps = float(kwargs['eps'])
self.beta = float(kwargs['beta'])
self.tau = float(kwargs['tau'])
self.n = int(kwargs['n'])
self.data = np.empty((self.n, 3))
self.Cl = 0.0
self.lower = None
self.upper = None
self.camber = None
self.thickness = None
self.dpan = True if 'dpan' in kwargs.keys() else False
def __call__(self, *args, **kwargs):
self._get_ktreff_data_matlab()
self._calc_lower_upper()
self._calc_camber()
self._calc_thickness()
if self.dpan:
self._get_doublet_data_matlab()
def _get_ktreff_data_matlab(self):
"""
Function to call MATLAB ktreff function and store data in object.
"""
eng = matlab.engine.start_matlab()
x, y, cp, cl = eng.ktreff(self.alpha, self.eps, self.beta, self.tau, float(self.n - 1), nargout=4)
self.data[:, 0] = x[0]
self.data[:, 1] = y[0]
self.data[:, 2] = cp[0]
self.Cl = cl
def _get_doublet_data_matlab(self):
"""
Function to call MATLAB dpan function and store data in object.
"""
x = matlab.double(self.data[:, 0].tolist())[0]
y = matlab.double(self.data[:, 1].tolist())[0]
eng = matlab.engine.start_matlab()
cp, cl = eng.dpan(float(self.n - 1), self.alpha, x, y, nargout=2)
self.dpan_cl = cl
self.dpan_cp = cp[0]
def get_excel(self):
"""
Function to write .xlsx file containing x, y, camber, thickness and Cp.
"""
data = pd.DataFrame(columns=['x', 'y', 'Cp'])
data['x'] = self.data[:, 0]
data['y'] = self.data[:, 1]
data['Cp'] = self.data[:, 2]
camber = pd.DataFrame(columns=['x', 'camber'])
camber['x'] = self.camber[:, 0]
camber['camber'] = self.camber[:, 1]
thickness = pd.DataFrame(columns=['thickness'])
thickness['thickness'] = self.thickness
return data, camber, thickness
def write_dat(self):
"""
Function to write .dat file containing x, y coordinates.
"""
data = self.get_data(True)
data.savetxt('{}.dat'.format(self.get_name()))
def get_data(self, coords_only):
"""
:param coords_only: True if only coordinate data required.
:return: Return array of data for aerofoil.
"""
return self.data[:, :-1] if coords_only else self.data
def _calc_lower_upper(self):
data = self.get_data(True)
lower = data[0:self.n/2]
upper = data[self.n/2:self.n]
self.lower = lower[lower[:, 0].argsort()][::-1]
self.upper = upper[upper[:, 0].argsort()][::-1]
def get_lower_upper(self):
return self.lower, self.upper
def _calc_camber(self):
self.camber = 0.5 * (self.lower + self.upper)
def get_camber(self):
return self.camber
def get_max_camber(self):
return self.camber[np.argmax(self.camber[:, 1])]
def _calc_thickness(self):
interp_upper = griddata(self.upper[:, 0], self.upper[:, 1], self.lower[:, 0], method='linear')
thickness = interp_upper - self.lower[:, 1]
thickness = thickness[np.where(np.logical_not(np.isnan(thickness)))]
self.thickness = thickness
def get_thickness(self):
return self.thickness
def get_max_thickness(self):
return np.max(self.thickness)
def get_naca_digits(self):
max_camber_x, max_camber = self.get_max_camber()
max_thickness = self.get_max_thickness()
return int(round(max_camber * 100)), int(round(max_camber_x * 10)), int(round(max_thickness * 100))
def get_name(self):
return 'ktreff(alpha={},eps={},beta={},tau={},n={})'.format(np.round(self.alpha * math.pi / 180.0, 1),
self.eps, self.beta, self.tau,
self.n)