#
# ADflow, multiblock structured flow solver
#
# This code solves the 3D RANS, laminar NS or Euler equations
# on multiblock structured hexahedral grids.
# This is a parallel executable running on 1 processors.
# It has been compiled with the following options:
# - Optimized mode.
# - Size of standard integers: 4 bytes.
# - Size of standard floating point types: 8 bytes.
# - With cgns support
# - With support for signals.
#
'+----------------------------------------+'
'|          All ADFLOW Options:           |'
'+----------------------------------------+'
{'adjointdivtol': 100000.0,
 'adjointl2convergence': 1e-06,
 'adjointl2convergenceabs': 1e-16,
 'adjointl2convergencerel': 1e-16,
 'adjointmaxiter': 500,
 'adjointmonitorstep': 10,
 'adjointsolver': 'GMRES',
 'adjointsubspacesize': 100,
 'adpc': False,
 'agmglevels': 1,
 'agmgnsmooth': 3,
 'alphafollowing': True,
 'alphamode': False,
 'altitudemode': False,
 'ankadpc': False,
 'ankasmoverlap': 1,
 'ankcfl0': 5.0,
 'ankcflcutback': 0.5,
 'ankcflexponent': 0.5,
 'ankcflfactor': 10.0,
 'ankcfllimit': 100000.0,
 'ankcflmin': 1.0,
 'ankconstcflstep': 0.4,
 'ankcoupledswitchtol': 1e-06,
 'ankinnerpreconits': 2,
 'ankjacobianlag': 10,
 'anklinearsolvetol': 0.05,
 'anklinresmax': 0.1,
 'ankmaxiter': 40,
 'anknsubiterturb': 1,
 'ankouterpreconits': 2,
 'ankpcilufill': 2,
 'ankpcupdatetol': 0.5,
 'ankphysicallstol': 0.2,
 'ankphysicallstolturb': 0.99,
 'anksecondordswitchtol': 0.0001,
 'ankstepfactor': 1.0,
 'ankstepmin': 0.01,
 'anksubspacesize': -1,
 'ankswitchtol': 1.0,
 'ankturbcflscale': 1.0,
 'ankturbkspdebug': False,
 'ankunsteadylstol': 1.0,
 'ankusefullvisc': True,
 'ankusematrixfree': True,
 'ankuseturbdadi': True,
 'applyadjointpcsubspacesize': 20,
 'applypcsubspacesize': 10,
 'approxpc': True,
 'asmoverlap': 1,
 'backgroundvolscale': 1.0,
 'betamode': False,
 'blocksplitting': True,
 'cavitationnumber': 1.4,
 'cfl': 0.5,
 'cflcoarse': 0.25,
 'cfllimit': 1.5,
 'closedsurfacefamilies': None,
 'coarsediscretization': 'central plus scalar dissipation',
 'computecavitation': False,
 'coupledsolution': False,
 'cutcallback': None,
 'debugzipper': False,
 'deltat': 0.01,
 'designsurfacefamily': None,
 'discretization': 'central plus scalar dissipation',
 'dissipationlumpingparameter': 6.0,
 'dissipationscalingexponent': 0.67,
 'eddyvisinfratio': 0.009,
 'equationmode': 'steady',
 'equationtype': 'RANS',
 'eulerwalltreatment': 'linear pressure extrapolation',
 'firstrun': True,
 'flowtype': 'external',
 'forcesastractions': True,
 'frozenturbulence': False,
 'globalpreconditioner': 'additive Schwarz',
 'gridfile': 'wing_vol.cgns',
 'gridprecision': 'double',
 'gridprecisionsurface': 'single',
 'ilufill': 2,
 'infchangecorrection': True,
 'innerpreconits': 1,
 'isosurface': {},
 'isovariables': [],
 'l2convergence': 1e-12,
 'l2convergencecoarse': 0.01,
 'l2convergencerel': 1e-16,
 'liftindex': 2,
 'limiter': 'van Albada',
 'loadbalanceiter': 10,
 'loadimbalance': 0.1,
 'localpreconditioner': 'ILU',
 'lowspeedpreconditioner': False,
 'machmode': False,
 'matrixordering': 'RCM',
 'maxl2deviationfactor': 1.0,
 'meshsurfacefamily': None,
 'mgcycle': 'sg',
 'mgstartlevel': -1,
 'monitorvariables': ['resrho', 'cl', 'cd'],
 'ncycles': 1000,
 'ncyclescoarse': 250,
 'nearwalldist': 0.1,
 'nkadpc': False,
 'nkasmoverlap': 1,
 'nkfixedstep': 0.25,
 'nkinnerpreconits': 1,
 'nkjacobianlag': 20,
 'nklinearsolvetol': 0.3,
 'nkls': 'cubic',
 'nkouterpreconits': 1,
 'nkpcilufill': 2,
 'nksubspacesize': 60,
 'nkswitchtol': 1e-05,
 'nkuseew': True,
 'nkviscpc': False,
 'nrefine': 10,
 'nrkreset': 5,
 'nsavesurface': 1,
 'nsavevolume': 1,
 'nsubiter': 1,
 'nsubiterturb': 5,
 'ntimestepscoarse': 48,
 'ntimestepsfine': 400,
 'numbersolutions': True,
 'outerpreconits': 3,
 'outputdirectory': '.',
 'outputsurfacefamily': 'allSurfaces',
 'overlapfactor': 0.9,
 'oversetloadbalance': True,
 'oversetpriority': {},
 'oversetprojtol': 1e-12,
 'oversetupdatemode': 'frozen',
 'partitionlikenproc': -1,
 'partitiononly': False,
 'pmode': False,
 'preconditionerside': 'right',
 'printiterations': True,
 'printtiming': True,
 'printwarnings': True,
 'qmode': False,
 'resaveraging': 'alternate',
 'restartadjoint': True,
 'restartfile': None,
 'restrictionrelaxation': 0.8,
 'rkreset': False,
 'rmode': False,
 'selfzipcutoff': 120.0,
 'sepsensoroffset': 0.0,
 'sepsensorsharpness': 10.0,
 'setmonitor': True,
 'skipafterfailedadjoint': True,
 'smoother': 'DADI',
 'smoothparameter': 1.5,
 'solutionprecision': 'single',
 'solutionprecisionsurface': 'single',
 'storerindlayer': True,
 'surfacevariables': ['cp', 'vx', 'vy', 'vz', 'mach'],
 'timeaccuracy': 2,
 'timeintegrationscheme': 'BDF',
 'timeintervals': 1,
 'timelimit': -1.0,
 'tsstability': False,
 'turbresscale': 10000.0,
 'turbulencemodel': 'SA',
 'turbulenceorder': 'first order',
 'turbulenceproduction': 'strain',
 'useale': True,
 'useanksolver': True,
 'useapproxwalldistance': True,
 'useblockettes': True,
 'usediagtspc': True,
 'useft2sa': True,
 'usegridmotion': False,
 'uselinresmonitor': False,
 'usematrixfreedrdw': True,
 'usenksolver': False,
 'useoversetwallscaling': False,
 'useqcr': False,
 'userotationsa': False,
 'usewallfunctions': False,
 'usezippermesh': True,
 'verifyextra': True,
 'verifyspatial': True,
 'verifystate': True,
 'vis2': 0.25,
 'vis2coarse': 0.5,
 'vis4': 0.0156,
 'viscoussurfacevelocities': True,
 'viscpc': False,
 'viscwalltreatment': 'constant pressure extrapolation',
 'volumevariables': ['resrho'],
 'walldistcutoff': 1e+20,
 'windaxis': False,
 'writesurfacesolution': True,
 'writetecplotsurfacesolution': True,
 'writevolumesolution': True,
 'zippersurfacefamily': None}
-> Alpha... 0.000000
#
#                      Warning
# Conversion factor from grid units to meter not specified and some blocks
# do not have units. It is assumed that the grid is given in meters.
#
#
# Specified load imbalance tolerance  0.100 acheived
# Continuing with  0.000 load imbalance for the cells and  0.000 for the faces
#
#
# Grid level: 1, Total number of cells: 193536
#
+--------------------------------------------------+
  CGNS Surface Families by Boundary Condition Type
+--------------------------------------------------+
| Wall Types           : wall
| Inflow Types :
| Outflow Types :
| Symmetry Types       : sym
| Farfield Types       : far
| Oveset Types         :
+--------------------------------------------------+
+--------------------------------------------------+
|
| Initialization Times:
|
| Library Load Time             :      0.054 sec
| Set Defaults Time             :      0.000 sec
| Base class init Time          :      0.002 sec
| Introductory Time             :      0.008 sec
| Partitioning Time             :      0.023 sec
| Preprocessing Time            :      3.098 sec
| Family Setup Time             :      0.000 sec
| Cut callback Time             :      0.000 sec
| Overset Preprocessing Time    :      0.001 sec
| Initialize Flow Time          :      0.032 sec
|
| Total Init Time               :      3.219 sec
+--------------------------------------------------+
Traceback (most recent call last):
  File "/usr/local/lib/python3.8/dist-packages/baseclasses/BaseSolver.py", line 115, in setOption
    defaultType, defaultValue = self.defaultOptions[name]
  File "/usr/local/lib/python3.8/dist-packages/baseclasses/utils.py", line 21, in __getitem__
    return super().__getitem__(key.lower())
KeyError: 'outputdirectory'

During handling of the above exception, another exception occurred:

Traceback (most recent call last):
  File "mphys_aero.py", line 99, in <module>
    prob.setup()
  File "/usr/local/lib/python3.8/dist-packages/openmdao/core/problem.py", line 904, in setup
    model._setup(model_comm, mode, self._metadata)
  File "/usr/local/lib/python3.8/dist-packages/openmdao/core/system.py", line 711, in _setup
    self._setup_procs(self.pathname, comm, mode, self._problem_meta)
  File "/usr/local/lib/python3.8/dist-packages/openmdao/core/group.py", line 591, in _setup_procs
    subsys._setup_procs(subsys.pathname, sub_comm, mode, prob_meta)
  File "/usr/local/lib/python3.8/dist-packages/openmdao/core/group.py", line 536, in _setup_procs
    self.setup()
  File "/home/user/.local/lib/python3.8/site-packages/mphys/multipoint.py", line 33, in setup
    self.aero_builder.init_solver(self.comm)
  File "/home/user/.local/lib/python3.8/site-packages/mphys/mphys_adflow.py", line 1029, in init_solver
    mesh = USMesh(options=self.options, comm=comm)
  File "/usr/local/lib/python3.8/dist-packages/idwarp/UnstructuredMesh.py", line 103, in __init__
    super().__init__(name, category, defaultOptions=defOpts, options=options, comm=comm)
  File "/usr/local/lib/python3.8/dist-packages/baseclasses/BaseSolver.py", line 88, in __init__
    self.setOption(key, options[key])
  File "/usr/local/lib/python3.8/dist-packages/baseclasses/BaseSolver.py", line 121, in setOption
    raise Error(f"Option {name} is not a valid {self.name} option. Perhaps you meant {guess}?")
baseclasses.utils.Error:
+------------------------------------------------------------------------------+
| Error: Option outputdirectory is not a valid IDWarp option. Perhaps you      |
| meant ldeffact?                                                              |
+------------------------------------------------------------------------------+

Exception ignored in: <function USMesh.__del__ at 0x7f8e218c8040>
Traceback (most recent call last):
  File "/usr/local/lib/python3.8/dist-packages/idwarp/UnstructuredMesh.py", line 1116, in __del__
    self.warp.releasememory()
AttributeError: 'USMesh' object has no attribute 'warp'