def test_ap_bcvar_nodal_array(self):
gridFile = os.path.join(baseDir, '../input_files/conic_conv_nozzle_mb_L4_array.cgns')
options = copy.deepcopy(self.options)
options['gridfile'] = gridFile
CFDSolver = ADFLOW(options=options)
CFDSolver.addFamilyGroup('upstream',['inlet'])
CFDSolver.addFamilyGroup('downstream',['outlet'])
ap = self.ap
group = 'outlet'
BCVar = 'Pressure'
# ap.bc_data = bc_data
ap.setBCVar(BCVar, 70000.0, group)
ap.addDV(BCVar, name='outlet_pressure', familyGroup=group,)
# DVs = {'outlet_pressure':123000.0}
DVs = {'outlet_pressure':np.arange(1,5*9+1)*10**5}
ap.setDesignVars(DVs)
assert (ap.getBCData()[group][BCVar] == DVs['outlet_pressure']).all()
CFDSolver.setAeroProblem(ap)
bc_data = CFDSolver.getBCData(groupNames=[group])
for ii, d in enumerate(bc_data.getBCArraysFlatData(BCVar, familyGroup=group)):
assert d == DVs['outlet_pressure'][ii]
def test_ap_bcvar_array(self):
CFDSolver = ADFLOW(options=self.options)
CFDSolver.addFamilyGroup('upstream',['inlet'])
CFDSolver.addFamilyGroup('downstream',['outlet'])
ap = self.ap
group = 'outlet'
BCVar = 'Pressure'
# ap.bc_data = bc_data
ap.setBCVar(BCVar, 70000.0, group)
ap.addDV(BCVar, name='outlet_pressure', familyGroup=group,)
# DVs = {'outlet_pressure':123000.0}
DVs = {'outlet_pressure':np.arange(1,6)*10**5}
ap.setDesignVars(DVs)
print(ap.getBCData()[group][BCVar] == DVs['outlet_pressure'])
assert (ap.getBCData()[group][BCVar] == DVs['outlet_pressure']).all()
CFDSolver.setAeroProblem(ap)
bc_data = CFDSolver.getBCData(groupNames=[group])
for ii, d in enumerate(bc_data.getBCArraysFlatData(BCVar, familyGroup=group)):
assert d == DVs['outlet_pressure'][ii]
def test_ap_bcvar_scalar(self):
CFDSolver = ADFLOW(options=self.options)
CFDSolver.addFamilyGroup('upstream',['inlet'])
CFDSolver.addFamilyGroup('downstream',['outlet'])
ap = self.ap
group = 'outlet'
BCVar = 'Pressure'
# ap.bc_data = bc_data
ap.setBCVar(BCVar, 70000.0, group)
ap.addDV(BCVar, name='outlet_pressure', familyGroup=group,)
DVs = {'outlet_pressure':123000.0}
ap.setDesignVars(DVs)
assert ap.getBCData()[group][BCVar] == DVs['outlet_pressure']
CFDSolver.setAeroProblem(ap)
bc_data = CFDSolver.getBCData(groupNames=[group])
for d in bc_data.getBCArraysFlatData(BCVar, familyGroup=group):
assert d == DVs['outlet_pressure']