Source code for pumapy.materialproperties.elasticity

from pumapy.physicsmodels.mpsa_elasticity import Elasticity
from pumapy.physicsmodels.property_maps import ElasticityMap
from scipy.optimize import fsolve
import numpy as np


[docs]def compute_elasticity(workspace, elast_map, direction, side_bc='p', prescribed_bc=None, tolerance=1e-4, maxiter=100000, solver_type='gmres', display_iter=True, print_matrices=(0, 0, 0, 0, 0)): """ Compute the effective elasticity coefficient (N.B. 0 material ID in workspace refers to air unless otherwise specified) :param workspace: domain :type workspace: pumapy.Workspace :param elast_map: local elasticity of the constituents :type elast_map: pumapy.ElasticityMap :param direction: direction for solve ('x','y', 'z', 'yz', 'xz', 'xy') :type direction: string :param side_bc: side boundary conditions can be symmetric ('s'), periodic ('p'), dirichlet ('d') or free ('f') :type side_bc: string :param prescribed_bc: 3D array holding dirichlet BC :type prescribed_bc: pumapy.ElasticityBC or None :param tolerance: tolerance for iterative solver :type: tolerance: float :param maxiter: maximum Iterations for solver :type maxiter: int :param solver_type: solver type, options: 'bicgstab', 'cg', 'gmres' (default), 'direct' :type solver_type: string :param display_iter: display iterations and residual :type display_iter: bool :param print_matrices: corresponding to b, E, A, u, s decimal places. If 0, they are not printed :type print_matrices: (int, int, int, int, int) :return: elasticity, displacement field, direct stresses (sigma xx, yy, zz), shear stresses (tau yz, xz, xy) :rtype: ((float, float, float, float, float, float), numpy.ndarray, numpy.ndarray, numpy.ndarray) :Example: >>> import pumapy as puma >>> ws = puma.Workspace.from_shape_value((20, 20, 20), 1) >>> ws[int(ws.matrix.shape[0] / 2):] = 2 >>> elast_map = puma.ElasticityMap() >>> elast_map.add_isotropic_material((1, 1), 200, 0.3) >>> elast_map.add_isotropic_material((2, 2), 400, 0.1) >>> C, u, s, t = puma.compute_elasticity(ws, elast_map, direction='x', side_bc='f', solver_type="direct") >>> print(C) """ if isinstance(elast_map, ElasticityMap): solver = Elasticity(workspace, elast_map, direction, side_bc, prescribed_bc, tolerance, maxiter, solver_type, display_iter, print_matrices) else: raise Exception("elast_map has to be an ElasticityMap") solver.error_check() solver.log_input() solver.compute() solver.log_output() return solver.Ceff, solver.u, solver.s, solver.t
[docs]def compute_stress_analysis(workspace, elast_map, prescribed_bc, side_bc='p', tolerance=1e-4, maxiter=100000, solver_type='gmres', display_iter=True, print_matrices=(0, 0, 0, 0, 0)): """ Compute stress analysis (N.B. 0 material ID in workspace refers to air unless otherwise specified) :param workspace: domain :type workspace: pumapy.Workspace :param elast_map: local elasticity of the constituents :type elast_map: pumapy.ElasticityMap :param prescribed_bc: 3D array holding dirichlet BC :type prescribed_bc: pumapy.ElasticityBC :param side_bc: side boundary conditions can be symmetric ('s'), periodic ('p'), dirichlet ('d') or free ('f') :type side_bc: string :param tolerance: tolerance for iterative solver :type tolerance: float :param maxiter: maximum Iterations for solver :type maxiter: int :param solver_type: solver type, options: 'bicgstab', 'cg', 'gmres' (default), 'direct' :type solver_type: string :param display_iter: display iterations and residual :type display_iter: bool :param print_matrices: corresponding to b, E, A, u, s decimal places. If 0, they are not printed :type print_matrices: (int, int, int, int, int) :return: displacement field, direct stresses (sigma xx, yy, zz), shear stresses (tau yz, xz, xy) :rtype: (numpy.ndarray, numpy.ndarray, numpy.ndarray) :Example: >>> import pumapy as puma >>> ws = puma.Workspace.from_shape_value((20, 20, 20), 1) >>> ws[ws.matrix.shape[0]//2:] = 2 >>> elast_map = puma.ElasticityMap() >>> elast_map.add_isotropic_material((1, 1), 200, 0.3) >>> elast_map.add_isotropic_material((2, 2), 400, 0.1) >>> bc = puma.ElasticityBC(ws) >>> bc.dirichlet[0] = 0 # hold x -ve face >>> bc.dirichlet[-1, :, :, 0] = 1 # displace x +ve face by 1 in x direction >>> bc.dirichlet[-1, :, :, 1:] = 0 # hold x +ve face in y and z directions >>> u, s, t = puma.compute_stress_analysis(ws, elast_map, bc, side_bc='f', solver_type="direct") >>> puma.render_volume(u[:, :, :, 1], cmap='jet') # displacement magnitude in y direction """ if isinstance(elast_map, ElasticityMap): solver = Elasticity(workspace, elast_map, None, side_bc, prescribed_bc, tolerance, maxiter, solver_type, display_iter, print_matrices) else: raise Exception("elast_map has to be an ElasticityMap") solver.error_check() solver.log_input() solver.compute() solver.log_output() return solver.u, solver.s, solver.t
[docs]def get_E_nu_from_elasticity(C11, C12, C13, C22, C23, C33): """ Compute Young's moduli E1, E2, E3 and Poisson's ratios nu12, nu23, nu31 from symmetric elastic stiffness tensor :param C11: elasticity tensor component :type C11: float :param C12: elasticity tensor component :type C12: float :param C13: elasticity tensor component :type C13: float :param C22: elasticity tensor component :type C22: float :param C23: elasticity tensor component :type C23: float :param C33: elasticity tensor component :type C33: float :return: Young's moduli E1, E2, E3 and Poisson's ratios nu12, nu23, nu31 :rtype: (float, float, float, float, float, float) """ def eqs(unknowns, *cs): E1, E2, E3, nu12, nu23, nu31 = unknowns c11, c12, c31, c22, c23, c33 = cs nu21 = nu12 * E2 / E1 nu32 = nu23 * E3 / E2 nu13 = nu31 * E1 / E3 c0 = (1 - nu12 * nu21 - nu23 * nu32 - nu13 * nu31 - 2 * nu21 * nu32 * nu13) / (E1 * E2 * E3) return (c11 - (1 - nu23 * nu32) / (c0 * E2 * E3), c22 - (1 - nu13 * nu31) / (c0 * E1 * E3), c33 - (1 - nu21 * nu12) / (c0 * E2 * E1), c12 - (nu12 + nu32 * nu13) / (c0 * E1 * E3), c23 - (nu23 + nu21 * nu13) / (c0 * E1 * E2), c31 - (nu31 + nu21 * nu32) / (c0 * E2 * E3)) s = fsolve(eqs, np.full(6, 0.1), args=(C11, C12, C13, C22, C23, C33)) [print(i, j) for i, j in zip(["E1", "E2", "E3", "nu12", "nu23", "nu31"], s)] return s