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import numpy as np
from materials import *
import matplotlib.pyplot as plt
import math
class motor_case():
def __init__(self, material_case, material_liner, insulator_thk, case_thk, ri, r_steps, hm, Tc, Ta,
burn_time, t_steps, type):
self.rho_case, self.k_case, self.cp_case = case_selector(material_case)
self.rho_insulator, self.k_insulator, self.cp_insulator = insulator_selector(material_liner)
self.insulator_thk = insulator_thk
self.case_thk = case_thk
self.r_1 = ri
self.sectionsr = r_steps
self.h_m = hm
self.Tc = Tc
self.Ta = Ta
self.t = burn_time
self.nt = t_steps
self.alpha_case = float(self.k_case / (self.cp_case * self.rho_case))
self.alpha_insulator = float(self.k_insulator / (self.cp_insulator * self.rho_insulator))
if type == 1:
self.T, self.Values = self.run_analysis_case()
elif type == 2:
self.T, self.Values = self.run_analysis_explicit()
def run_analysis_case(self):
# Radial coordinate
self.r_2 = self.r_1 + self.insulator_thk # Radial position of insulation/casing interface [m]
self.r_3 = self.r_2 + self.case_thk # Radial position of casing end [m]
self.dr = (self.r_3 - self.r_1) / self.sectionsr # r variation [m]
self.nr = self.sectionsr + 1 # Nº of radial points
# Time
self.dt = self.t / self.nt # Time variation [s]
# we have to set the initial and boundary conditions
self.r = [self.r_1 + i * self.dr for i in range(self.nr)] # Defining the r vector
A = self.create_Amatrix()
# Creating the T matrix
T_implicit = np.zeros([self.nt, self.nr])
# Setting initial values for the T matrix
for i in range(self.nr):
T_implicit[0][i] = self.Ta
# Getting the inverse matrix of A
A_inverse = np.linalg.inv(A)
# Calculating the implicit T matrix
for i in range(self.nt - 1):
T_implicit[i][0] = T_implicit[i][0] + (self.h_m*2*self.dt*(self.Tc-T_implicit[i][0]))/(self.rho_insulator*self.cp_insulator*self.dr)
T_implicit[i + 1] = (np.matmul(A_inverse, T_implicit[i]))
values = T_implicit[self.nt-1, ::]
return T_implicit, values
def run_analysis_explicit(self):
# Radial coordinate
self.r_2 = self.r_1 + self.insulator_thk # Radial position of insulation/casing interface [m]
self.r_3 = self.r_2 + self.case_thk # Radial position of casing end [m]
self.dr = (self.r_3 - self.r_1) / self.sectionsr # r variation [m]
self.nr = self.sectionsr + 1 # Nº of radial points
# Time
self.dt = self.dr ** 2 / (2 * self.alpha_case) # Time variation [s]
self.nt_ex = self.nr
# we have to set the initial and boundary conditions
self.r = [self.r_1 + i * self.dr for i in range(self.nr)] # Defining the r vector
d_insulator = self.alpha_insulator * (self.dt / (self.dr ** 2)) # Insulation Fourier number
d_case = self.alpha_case * (self.dt / (self.dr ** 2)) # Casing Fourier number
if d_insulator > 0.5 or d_case > 0.5:
print('Stability criteria was not achieved, the following values must be less than 0.5')
print('Fourier number case: ', d_case)
print('Fourier number insulator: ', d_insulator)
print('Try to decrease the radial steps')
return 0
T = np.zeros([self.nt_ex, self.nr])
for i in range(self.nr):
T[0][i] = self.Ta
# Calculating the T-matrix
for j in range(self.nt_ex - 1):
for i in range(self.nr):
if self.r[i] < self.r_2: # EPDM
alpha = self.alpha_insulator
rho = self.rho_insulator
cp = self.cp_insulator
k = self.k_insulator
if self.r[i] >= self.r_2: # Corrections are needed here
alpha = self.alpha_case
rho = self.rho_case
cp = self.cp_case
k = self.k_case
if i == self.nr - 1:
T[j + 1][i] = T[j][i] + alpha * self.dt * (
((1 / (self.r[i] * self.dr)) * (T[j][i] - T[j][i - 1])) + (
(T[j][i] + T[j][i - 2] - 2 * T[j][i - 1]) /
(self.dr ** 2)))
elif i == 0:
T[j + 1][i] = T[j][i] + (2 / (rho * cp * self.dr)) * (
self.h_m * self.dr * (self.Tc - T[j][0]) + k * (T[j][1] - T[j][0]))
else:
T[j + 1][i] = T[j][i] + alpha * self.dt * (
((1 / (2 * self.r[i] * self.dr)) * (T[j][i + 1] - T[j][i - 1])) + (
(T[j][i + 1] + T[j][i - 1] - 2 * T[j][i]) /
(self.dr ** 2)))
values = T[self.nt_ex - 1, ::]
return T, values
def create_Amatrix(self):
# Creating the A matrix
A = np.zeros([self.nr, self.nr])
# Building the A matrix
A[0][0] = 1 + (2 * self.dt * self.k_insulator) / (self.rho_insulator * self.cp_insulator * self.dr ** 2)
A[0][1] = -self.k_insulator * 2 * self.dt / (self.dr * self.dr * self.rho_insulator * self.cp_insulator)
A[self.nr - 1][self.nr - 1] = 1 - self.alpha_case * self.dt / (self.r[self.nr - 1] * self.dr) - self.alpha_case * self.dt / (self.dr ** 2)
A[self.nr - 1][self.nr - 2] = self.alpha_case * self.dt / (self.r[self.nr - 1] * self.dr) + 2 * self.alpha_case * self.dt / (self.dr ** 2)
A[self.nr - 1][self.nr - 3] = -self.alpha_case * self.dt / (self.dr ** 2)
for i in range(1, self.nr - 1):
if self.r[i] >= self.r_2:
alpha = self.alpha_case
else:
alpha = self.alpha_insulator
A[i][i - 1] = -(alpha * self.dt) / (self.dr ** 2) + alpha * self.dt / (2 * self.dr * self.r[i])
A[i][i] = 1 + 2 * alpha * self.dt / (self.dr ** 2)
A[i][i + 1] = -(alpha * self.dt) / self.dr ** 2 - alpha * self.dt / (2 * self.dr * self.r[i])
return A
class bulkhead(object):
def __init__(self, material_case, material_liner, insulator_thk, bulkhead_thk, radius_inner, radius_outer, burn_time, sectionsr, hm, Ta, Tc ):
# Explicit atributes for bulkhead
self.rho_case, self.k_case, self.cp_case = case_selector(material_case) # Case properties
self.rho_insulator, self.k_insulator, self.cp_insulator = insulator_selector(material_liner) # Insulator properties
self.h_m = hm
self.insulator_thk = insulator_thk
self.z = bulkhead_thk
self.radius_inner = radius_inner
self.radius_outer = radius_outer
self.t = burn_time
self.sectionsr = sectionsr
self.Ta = Ta
self.Tc = Tc
self.alpha_case = float(self.k_case/(self.cp_case*self.rho_case))
self.alpha_insulator = float(self.k_insulator / (self.cp_insulator * self.rho_insulator))
self.T_bulkhead = self.run_analysis_bulkhead()
def run_analysis_bulkhead(self):
nr = self.sectionsr + 1
dr = (self.radius_outer) / self.sectionsr # r variation [m]
r_1 = dr # Radial position of insulation beginning [m]
r_2 = r_1 + self.radius_inner # Radial position of insulation/casing interface [m]
r_3 = self.radius_outer # Radial position of casing end [m]
z_1 = 0
z_2 = self.insulator_thk
z_3 = z_2 + self.z
dz = dr / 1.4 # z variation [m]
nz = math.ceil(self.z / dz) # Nº of z points
dt = ((dr ** 2) * (dz ** 2)) / (1.99 * self.alpha_case * (dr ** 2 + dz ** 2))
nt = math.ceil(self.t / dt)
d_insulator = self.alpha_insulator * (dt / (dr ** 2)) # Insulation Fourier number
d_case = self.alpha_case * (dt / (dr ** 2)) # Casing Fourier number
# we have to set the initial/boundary contitions
r = [r_1 + i * dr for i in range(nr)]
z = [z_1 + i * dz for i in range(nz)]
T = np.zeros([nt, nr, nz])
for i in range(nr):
for j in range(nz):
T[0][i][j] = self.Ta
# Calculating the T-matrix
for i in range(nt - 1):
for l in range(nz):
for j in range(nr):
if z[l] <= z_2: # Set insulation material
alpha = self.alpha_insulator
rho = self.rho_insulator
cp = self.cp_insulator
k = self.k_insulator
if z[l] > z_2: # Set casing material
alpha = self.alpha_case
rho = self.rho_case
cp = self.cp_case
k = self.k_case
if l == nz - 1:
if j == nr - 1: # z end and r end
T[i + 1][j][l] = (1 + (alpha * dt) / (r[j] * dr) + (alpha * dt) / (dr ** 2) + (
alpha * dt) / (dz ** 2)) * T[i][j][l] + (
(-2 * alpha * dt) / (dr ** 2) - (alpha * dt) / (r[j] * dr)) * \
T[i][j - 1][l] + ((alpha * dt) / (dr ** 2)) * T[i][j - 2][l] + (
(-2 * alpha * dt) / (dz ** 2)) * T[i][j][l - 1] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l - 2]
elif j == 0: # z end and r start
T[i + 1][j][l] = (1 - (alpha * dt) / (r[j] * dr) + (alpha * dt) / (dr ** 2) + (
alpha * dt) / (dz ** 2)) * T[i][j][l] + (
(alpha * dt) / (r[j] * dr) - (2 * alpha * dt) / (dr ** 2)) * \
T[i][j + 1][l] + ((alpha * dt) / (dr ** 2)) * T[i][j + 2][l] + (
(-2 * alpha * dt) / (dz ** 2)) * T[i][j][l - 1] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l - 2]
else: # z end and r middle
T[i + 1][j][l] = (1 - (2 * alpha * dt) / (dr ** 2) + (alpha * dt) / (dz ** 2)) * T[i][j][
l] + ((alpha * dt) / (dr ** 2) - (alpha * dt) / (2 * r[j] * dr)) * T[i][j - 1][l] + (
(alpha * dt) / (dr ** 2) + (alpha * dt) / (2 * r[j] * dr)) * \
T[i][j + 1][l] + ((-2 * alpha * dt) / (dz ** 2)) * T[i][j][l - 1] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l - 2]
elif l == 0:
if j == nr - 1: # z start and r end
T[i + 1][j][l] = (2 * self.h_m * dt * Tc) / (rho * cp * dz) + (
1 + (k * dt) / (rho * cp * (dr) ** 2) - (k * dt) / (rho * cp * (dz) ** 2) - (
2 * self.h_m * dt) / (rho * cp * dz)) * T[i][j][l] + (
(-k * dt) / (rho * cp * (dr) ** 2)) * T[i][j - 1][l] + (
(k * dt) / (rho * cp * (dz) ** 2)) * T[i][j][l + 1]
elif j == 0: # z start and r start
T[i + 1][j][l] = (2 * self.h_m * dt * Tc) / (rho * cp * dz) + (
1 - (k * dt) / (rho * cp * (dr) ** 2) - (k * dt) / (rho * cp * (dz) ** 2) - (
2 * self.h_m * dt) / (rho * cp * dz)) * T[i][j][l] + (
(k * dt) / (rho * cp * (dr) ** 2)) * T[i][j + 1][l] + (
(k * dt) / (rho * cp * (dz) ** 2)) * T[i][j][l + 1]
else: # z start and r middle
T[i + 1][j][l] = (2 * self.h_m * dt * Tc) / (rho * cp * dz) + (
1 - (k * dt) / (rho * cp * (dz) ** 2) - (2 * self.h_m * dt) / (rho * cp * dz)) * \
T[i][j][l] + ((k * dt) / (rho * cp * (dr) ** 2)) * T[i][j + 1][l] + (
(-k * dt) / (rho * cp * (dr) ** 2)) * T[i][j - 1][l] + (
(k * dt) / (rho * cp * (dz) ** 2)) * T[i][j][l + 1]
else:
if j == nr - 1: # z middle and r end
T[i + 1][j][l] = (1 + (alpha * dt) / (r[j] * dr) + (alpha * dt) / (dr ** 2) - (
2 * alpha * dt) / (dz ** 2)) * T[i][j][l] + (
(-2 * alpha * dt) / (dr ** 2) - (alpha * dt) / (r[j] * dr)) * \
T[i][j - 1][l] + ((alpha * dt) / (dr ** 2)) * T[i][j - 2][l] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l - 1] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l + 1]
elif j == 0: # z middle and r start
T[i + 1][j][l] = (1 - (alpha * dt) / (r[j] * dr) + (alpha * dt) / (dr ** 2) - (
2 * alpha * dt) / (dz ** 2)) * T[i][j][l] + (
(alpha * dt) / (r[j] * dr) - (2 * alpha * dt) / (dr ** 2)) * \
T[i][j + 1][l] + ((alpha * dt) / (dr ** 2)) * T[i][j + 2][l] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l - 1] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l + 1]
else: # z middle and r middle
T[i + 1][j][l] = (1 - (2 * alpha * dt) / (dr ** 2) - (2 * alpha * dt) / (dz ** 2)) * \
T[i][j][l] + ((alpha * dt) / (dr ** 2) - (alpha * dt) / (2 * r[j] * dr)) * \
T[i][j - 1][l] + (
(alpha * dt) / (dr ** 2) + (alpha * dt) / (2 * r[j] * dr)) * \
T[i][j + 1][l] + ((alpha * dt) / (dz ** 2)) * T[i][j][l - 1] + (
(alpha * dt) / (dz ** 2)) * T[i][j][l + 1]
self.t1 = int(nt*0.25)
self.t2 = int(nt*0.5)
self.t3 = int(nt*0.75)
self.t4 = int(nt-1)
return T
if __name__ == "__main__":
# CASING ANALYSIS
material_case = 'Aluminum 6061 - T6' # Case material ['aluminium6061t6']
material_liner = 'EPDM' # Insulator Material ['epdm']
ri = 0.11 # Initial cylinder radius
insulatior_thk = 0.003 # Insulator thickness
case_thk = 0.00555 # Case thickness
r_steps = 100 # Radial steps
hm = 1295 # Average convection coefficient
Tc = 1600 # Combustion chamber temperature
Ta = 297 # Ambient temperature
burn_time = 5 # Burn time
t_steps = 500 # time steps
"""
type = 2
motor1 = motor_case(material_case, material_liner, insulatior_thk, case_thk, ri, r_steps, hm, Tc, Ta, burn_time, t_steps, type)
print(motor1.T)
# Building graphs
r_a = np.array(motor.r)
locals = [r_a >= motor.r_2]
r_a = r_a[tuple(locals)]
fig, ax = plt.subplots(figsize=(10,25))
ax.plot(r_a, motor.Values[motor.r.index(r_a[0])::], 'r-+', linewidth=2, label='Implicit Method')
ax.plot(r_a, motor1.Values[motor.r.index(r_a[0])::], 'b', linewidth=2, label='Explicit Method')
ax.set_title('Temperature distribuition along the case - Insulation tichkness: ' + str(insulatior_thk*1000) + ' mm')
ax.set_xlabel('Radial position [m]')
ax.set_ylabel('Temperature [K]')
ax.legend()
plt.show()
"""
import pandas as pd
# BULKHEAD ANALYSIS
radius_inner = 0.064
radius_outer = 0.07
bulkhead_thk = 0.007
bulk = bulkhead(material_case, material_liner, insulatior_thk, bulkhead_thk, radius_inner, radius_outer, burn_time, r_steps, hm, Ta, Tc)
data = pd.DataFrame(data=bulk.T_bulkhead[bulk.t1,:,:])
print(data)