dragonfly_sim.core.postprocessor
Classes
Module Contents
- class dragonfly_sim.core.postprocessor.DG_postprocessor(Mesh_obj, sim_model, wall_meshtag_val, aero_center, ref_area_dim=None, ref_chord_dim=None, testing_mode=False, linear_solver_rtol=1e-16, linear_solver_atol=1e-11, linear_solver_max_it=1000, linear_residual_accept_limit=1e-10, p_inf_dim=None, L_ref_dim=1.0)
Bases:
csdl_alpha.CustomExplicitOperation- _assemble_mesh_derivative(form, label)
- _assemble_state_derivative(form, label)
- _assemble_value_and_coefficient(form, normalizer)
- _compute_S_ref()
- _compute_chord_ref(S_ref_value)
- _pressure_force_vector(u_dof_vec)
- compute(input_vals, output_vals)
- compute_D_deriv(u_dof_vec)
- compute_D_meshderiv(u_dof_vec)
- compute_L_deriv(u_dof_vec)
- compute_L_meshderiv(u_dof_vec)
- compute_M_deriv(u_dof_vec)
- compute_M_meshderiv(u_dof_vec)
- compute_cd(u_dof_vec)
- compute_cl(u_dof_vec)
- compute_cm(u_dof_vec)
- compute_cm_alpha(u_dof_vec)
- compute_cm_deriv(u_dof_vec)
- compute_derivatives(input_vals, outputs_vals, derivatives)
- compute_force_in_direction(u_dof_vec, direction_vec)
- compute_initial_and_constant_quantities()
- compute_moment_form(u_dof_vec)
- evaluate(u_vec, mesh_deformation, alpha, shape_param_inputs=None)
- refresh_geometry_dependent_reference_quantities()
- set_angle_of_attack(alpha)
- L_ref_dim = 1.0
- aero_center
- linear_residual_accept_limit = 1e-10
- linear_solver_atol = 1e-11
- linear_solver_max_it = 1000
- linear_solver_rtol = 1e-16
- log_cm_alpha = True
- mesh_obj
- ordered_callbacks = True
- p_inf_dim = None
- ref_area_dim = None
- ref_chord_dim = None
- sim_model
- testing_mode = False
- wall_meshtag_val