def setup(self):
surface = self.options['surface']
self.add_subsystem('nodes',
ComputeNodes(surface=surface),
promotes_inputs=['mesh'], promotes_outputs=['nodes'])
self.add_subsystem('assembly',
AssembleKGroup(surface=surface),
promotes_inputs=['A', 'Iy', 'Iz', 'J', 'nodes'], promotes_outputs=['local_stiff_transformed'])
self.add_subsystem('structural_mass',
Weight(surface=surface),
promotes_inputs=['A', 'nodes'],
promotes_outputs=['structural_mass', 'element_mass'])
self.add_subsystem('structural_cg',
StructuralCG(surface=surface),
promotes_inputs=['nodes', 'structural_mass', 'element_mass'],
promotes_outputs=['cg_location'])
if surface['fem_model_type'] == 'wingbox':
self.add_subsystem('fuel_vol',
WingboxFuelVol(surface=surface),
promotes_inputs=['nodes', 'A_int'],
promotes_outputs=['fuel_vols'])
def test(self):
surface = get_default_surfaces()[0]
group = om.Group()
comp = StructuralCG(surface=surface)
indep_var_comp = om.IndepVarComp()
ny = surface['mesh'].shape[1]
indep_var_comp.add_output('nodes', val=np.random.random((ny, 3)), units='m')
indep_var_comp.add_output('structural_mass', val=1., units='kg')
indep_var_comp.add_output('element_mass', val=np.ones((ny-1)), units='kg')
group.add_subsystem('indep_var_comp', indep_var_comp, promotes=['*'])
group.add_subsystem('structural_cg', comp, promotes=['*'])
run_test(self, group, complex_flag=True, compact_print=False)
def test(self):
surface = get_default_surfaces()[0]
group = Group()
comp = StructuralCG(surface=surface)
indep_var_comp = IndepVarComp()
ny = surface['num_y']
indep_var_comp.add_output('nodes', val=np.ones((ny, 3)), units='m')
indep_var_comp.add_output('structural_weight', val=1., units='N')
indep_var_comp.add_output('element_weights',
val=np.ones((ny - 1)),
units='N')
group.add_subsystem('indep_var_comp', indep_var_comp, promotes=['*'])
group.add_subsystem('structural_cg', comp, promotes=['*'])
run_test(self, group, complex_flag=True)
def setup(self):
surface = self.options['surface']
self.add_subsystem('nodes',
ComputeNodes(surface=surface),
promotes_inputs=['mesh'],
promotes_outputs=['nodes'])
self.add_subsystem('assembly',
AssembleK(surface=surface),
promotes_inputs=['A', 'Iy', 'Iz', 'J', 'nodes'],
promotes_outputs=['K'])
self.add_subsystem(
'structural_weight',
Weight(surface=surface),
promotes_inputs=['A', 'nodes', 'load_factor'],
promotes_outputs=['structural_weight', 'element_weights'])
self.add_subsystem(
'structural_cg',
StructuralCG(surface=surface),
promotes_inputs=['nodes', 'structural_weight', 'element_weights'],
promotes_outputs=['cg_location'])