Update X-HALE case
@@ -1669,7 +1669,6 @@ for case in cases:
'num_load_steps': 1,
'delta_curved': 1e-1,
'min_delta': tolerance,
- 'balancing': 'off',
'gravity_on': gravity,
'gravity': gravity_value}
@@ -1750,23 +1749,18 @@ for case in cases:
'thrust_nodes': thrust_nodes}
settings['StepUvlm'] = {'print_info': 'off',
- 'horseshoe': horseshoe,
'num_cores': 6,
- 'n_rollup': 0,
'convection_scheme': 2,
- 'rollup_dt': dt,
- 'rollup_aic_refresh': 1,
- 'rollup_tolerance': 1e-4,
'gamma_dot_filtering': 6,
# this is where the gust is input.
'velocity_field_generator': 'GustVelocityField',
'velocity_field_input': {'u_inf': u_inf,
'u_inf_direction': [1., 0, 0],
'gust_shape': gust_shape,
+ 'gust_parameters': {
'gust_length': gust_length,
- 'gust_intensity': gust_intensity*u_inf,
- 'offset': -space_offset,
- 'span': span_main},
+ 'gust_intensity': gust_intensity * u_inf},
+ 'offset': -space_offset},
'rho': rho,
'n_time_steps': n_tstep,
'dt': dt}
@@ -1847,13 +1841,11 @@ for case in cases:
'NumLambda': 100,
'write_modes_vtk': 'on',
'print_matrices': 'on',
- 'write_data': 'on',
'continuous_eigenvalues': 'off',
'dt': dt,
'plot_eigenvalues': 'on'}
settings['BeamPlot'] = {'include_rbm': 'on',
- 'include_applied_forces': 'on',
- 'include_forward_motion': 'off'}
+ 'include_applied_forces': 'on'}
settings['AerogridPlot'] = {'include_rbm': 'on',
'include_forward_motion': 'off',
