flying wings update
@@ -491,24 +491,24 @@ class FlyingWing():
# 'velocity_field_input': {'turbulent_field': '/2TB/turbsim_fields/TurbSim_wide_long_A_low.h5',
# 'offset': [30., 0., -10],
# 'u_inf': 0.},
- 'velocity_field_generator': 'GustVelocityField',
- 'velocity_field_input': {'u_inf': self.u_inf,
- 'u_inf_direction': self.u_inf_direction,
- 'gust_shape': 'continuous_sin',
- 'gust_length': self.gust_length,
- 'gust_intensity': self.gust_intensity * self.u_inf,
- 'offset': 15.0,
- 'span': self.main_chord * self.aspect_ratio},
- # 'velocity_field_generator': 'SteadyVelocityField',
- # 'velocity_field_input': {'u_inf': self.u_inf*1,
- # 'u_inf_direction': [1., 0., 0.]},
+ # 'velocity_field_generator': 'GustVelocityField',
+ # 'velocity_field_input': {'u_inf': self.u_inf,
+ # 'u_inf_direction': self.u_inf_direction,
+ # 'gust_shape': 'continuous_sin',
+ # 'gust_length': self.gust_length,
+ # 'gust_intensity': self.gust_intensity * self.u_inf,
+ # 'offset': 15.0,
+ # 'span': self.main_chord * self.aspect_ratio},
+ 'velocity_field_generator': 'SteadyVelocityField',
+ 'velocity_field_input': {'u_inf': self.u_inf*1,
+ 'u_inf_direction': [1., 0., 0.]},
'rho': self.rho,
'n_time_steps': self.n_tstep,
'dt': self.dt,
'gamma_dot_filtering': 3}
config['DynamicCoupled'] = {'print_info': 'on',
- 'structural_substeps': 1,
+ 'structural_substeps': 0,
'dynamic_relaxation': 'on',
'clean_up_previous_solution': 'on',
'structural_solver': 'NonLinearDynamicPrescribedStep',
@@ -523,7 +523,7 @@ class FlyingWing():
'final_relaxation_factor': 0.0,
'n_time_steps': self.n_tstep,
'dt': self.dt,
- 'include_unsteady_force_contribution': 'on',
+ 'include_unsteady_force_contribution': 'off',
'postprocessors': ['BeamLoads', 'StallCheck', 'BeamPlot', 'AerogridPlot'],
'postprocessors_settings': {'BeamLoads': {'folder': self.route + '/output/',
'csv_output': 'off'},
