def setup(self):
surface = self.options['surface']
promotes = []
if surface['struct_weight_relief']:
promotes = promotes + list(
set(['nodes', 'element_weights', 'load_factor']))
if surface['distributed_fuel_weight']:
promotes = promotes + list(set(['nodes', 'load_factor']))
self.add_subsystem('struct_states',
SpatialBeamStates(surface=surface),
promotes_inputs=['K', 'forces', 'loads'] + promotes,
promotes_outputs=['disp'])
self.add_subsystem('def_mesh',
DisplacementTransferGroup(surface=surface),
promotes_inputs=['nodes', 'mesh', 'disp'],
promotes_outputs=['def_mesh'])
self.add_subsystem('aero_geom',
VLMGeometry(surface=surface),
promotes_inputs=['def_mesh'],
promotes_outputs=[
'b_pts', 'widths', 'cos_sweep', 'lengths',
'chords', 'normals', 'S_ref'
])
self.linear_solver = LinearRunOnce()
def setup(self):
surface = self.options['surface']
promotes = []
if surface['struct_weight_relief']:
promotes = promotes + list(
set(['nodes', 'element_mass', 'load_factor']))
if surface['distributed_fuel_weight']:
promotes = promotes + list(set(['nodes', 'load_factor']))
if 'n_point_masses' in surface.keys():
promotes = promotes + list(
set([
'point_mass_locations', 'point_masses', 'nodes',
'load_factor', 'engine_thrusts'
]))
self.add_subsystem(
'struct_states',
SpatialBeamStates(surface=surface),
promotes_inputs=['local_stiff_transformed', 'forces', 'loads'] +
promotes,
promotes_outputs=['disp'])
self.add_subsystem('def_mesh',
DisplacementTransferGroup(surface=surface),
promotes_inputs=['nodes', 'mesh', 'disp'],
promotes_outputs=['def_mesh'])
normals_name = 'undeflected_normals'
self.add_subsystem('aero_geom',
VLMGeometry(surface=surface),
promotes_inputs=['def_mesh'],
promotes_outputs=[
'b_pts', 'widths', 'cos_sweep', 'lengths',
'chords', ('normals', normals_name), 'S_ref'
])
# Add control surfaces
if 'control_surfaces' in surface:
for ctrl_surf in surface['control_surfaces']:
#TODO: fixed name only works with one control surface
deflected_normals_name = "normals" #"{}_normals".format(ctrl_surf['name'])
self.add_subsystem(
ctrl_surf['name'],
ControlSurface(surface=surface,
panels=ctrl_surf['panels']),
promotes_inputs=[('normals', normals_name), 'delta_aileron'
], #,f"delta_{control_surf['name']}"],
promotes_outputs=[('deflected_normals',
deflected_normals_name)])
#iterate through names
normals_name = deflected_normals_name
else:
pass #No control surface to add
#self.connect(normals_name,'normals')
self.linear_solver = LinearRunOnce()
def setup(self):
surface = self.options['surface']
promotes = []
if surface['struct_weight_relief']:
promotes = promotes + list(
set(['nodes', 'element_mass', 'load_factor']))
if surface['distributed_fuel_weight']:
promotes = promotes + list(set(['nodes', 'load_factor']))
if 'n_point_masses' in surface.keys():
promotes = promotes + list(
set([
'point_mass_locations', 'point_masses', 'nodes',
'load_factor', 'engine_thrusts'
]))
self.add_subsystem(
'struct_states',
SpatialBeamStates(surface=surface),
promotes_inputs=['local_stiff_transformed', 'forces', 'loads'] +
promotes,
promotes_outputs=['disp'])
self.add_subsystem('def_mesh',
DisplacementTransferGroup(surface=surface),
promotes_inputs=['nodes', 'mesh', 'disp'],
promotes_outputs=['def_mesh'])
self.add_subsystem('aero_geom',
VLMGeometry(surface=surface),
promotes_inputs=['def_mesh'],
promotes_outputs=[
'b_pts', 'widths', 'cos_sweep', 'lengths',
'chords', 'S_ref'
])
# Add control surfaces
if 'control_surfaces' in surface:
self.add_subsystem(
'control_surfaces',
ControlSurfacesGroup(
control_surfaces=surface['control_surfaces'],
mesh=surface['mesh']),
promotes_inputs=['def_mesh'])
self.linear_solver = om.LinearRunOnce()