예제 #1
0
    def compute_initial_expansion_fan(self):
        M_max = gd.PR_expansion_mach(self.PR, self.gamma)
        # print('M_max: ' + str(M_max))
        mach_fan = np.linspace(1.1, M_max, self.n)

        (T_ratio, p_ratio, rho_ratio,
         a_ratio) = gd.isentropic_ratios(0, mach_fan, self.gamma)

        V_fan = a_ratio * self.spike.a_c * mach_fan

        W_fan = V_fan / self.V_l

        theta_fan = -gd.prandtl_meyer(mach_fan, self.gamma) + self.slope_init

        angle_fan = gd.mach_angle(mach_fan)

        # print(180/np.pi*np.arcsin(np.sqrt((gamma-1)/2*(1/W_fan**2-1))))
        # print(W_fan)

        # print(angle_fan*180/np.pi)

        x_fan = np.ones(angle_fan.shape) * self.spike.lip_x

        y_fan = np.ones(angle_fan.shape) * self.spike.lip_y

        #print(theta_fan*180/np.pi)
        # print(gd.mach_angle_velocity_ratio(gd.prandtl_meyer(2.3,gamma),0.3,gamma))

        initial_point = self.contour_point(chr_point(self.gamma, x_fan[0],
                                                     y_fan[0], theta_fan[0],
                                                     W_fan[0], 'N/A'),
                                           plot_chr=self.plot_chr)
        self.ID += 1
        self.ID_contour_chr.pop(0)
        self.chr_array = np.append(self.chr_array, initial_point)

        for point in x_fan[1:-1]:
            temp_point = chr_point(self.gamma, x_fan[self.ID], y_fan[self.ID],
                                   theta_fan[self.ID], W_fan[self.ID], 'N/A')
            new_point = self.general_point(temp_point,
                                           self.chr_array[self.ID - 1],
                                           plot_chr=self.plot_chr)
            # adding to arrays
            self.chr_array = np.append(self.chr_array, new_point)
            self.ID += 1

        first_jet = chr_point(self.gamma, x_fan[-1], y_fan[-1], theta_fan[-1],
                              W_fan[-1], 'N/A')
        second_jet = self.jet_boundary_point(first_jet,
                                             self.chr_array[self.ID - 1],
                                             plot_chr=self.plot_chr)
        self.chr_array = np.append(self.chr_array, second_jet)
        #self.ID_jet_boundary.append(self.ID)
        self.ID += 1
        self.add_break_ID()
    def design_nozzle(self):
        # discrete contour design variables
        self.M = np.linspace(1, self.M_e, self.n)
        self.A = self.A_t * gd.expansion_ratio(1, self.M, self.gamma)
        self.alpha = gd.prandtl_meyer(self.M_e, self.gamma) - gd.prandtl_meyer(
            self.M, self.gamma) + gd.mach_angle(self.M)
        self.l = (self.r_e - np.sqrt(
            np.abs(self.r_e**2 -
                   (self.A * self.M * np.sin(self.alpha) / np.pi)))) / np.sin(
                       self.alpha)

        self.x = self.l * np.cos(self.alpha)
        self.y = self.l * np.sin(self.alpha)

        self.centre_spike()

        self.length = self.x.max()