"author": "Aidan Jungo",
"email": "*****@*****.**",
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ----- Input -----
cpacs_inout.add_input(
var_name='nb_proc',
var_type=int,
default_value=1,
unit='1',
descr='Number of proc to use to run SU2',
xpath=CEASIOM_XPATH + '/aerodynamics/su2/settings/nbProc',
gui=True,
gui_name='Nb of processor',
gui_group='CPU',
)
cpacs_inout.add_input(
var_name='su2_mesh_path',
var_type='pathtype',
default_value='-',
unit='1',
descr='Absolute path of the SU2 mesh',
xpath=CEASIOM_XPATH + '/filesPath/su2Mesh',
gui=True,
gui_name='SU2 Mesh',
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
include_gui = False
# ----- Input -----
cpacs_inout.add_input(
var_name='sumo_file_path',
var_type='pathtype',
default_value='-',
unit='1',
descr='Absolute path to the SUMO file',
xpath=CEASIOM_XPATH + '/filesPath/sumoFilePath',
gui=True,
gui_name='SUMO File path',
gui_group='Inputs',
)
# ----- Output -----
cpacs_inout.add_output(
var_name='su2_mesh_path',
var_type='pathtype',
default_value=None,
unit='1',
descr='Absolute path of the SU2 mesh',
xpath=CEASIOM_XPATH + '/filesPath/su2Mesh',
REFS_XPATH = AIRCRAFT_XPATH + '/model/reference'
WING_XPATH = AIRCRAFT_XPATH + '/model/wings'
XPATH_PYTORNADO = '/cpacs/toolspecific/pytornado'
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
#===== Input =====
cpacs_inout.add_input(
var_name='',
var_type=list,
default_value=None,
unit=None,
descr="Name of the aero map to evaluate",
xpath=XPATH_PYTORNADO + '/aeroMapUID',
gui=True,
gui_name='__AEROMAP_SELECTION',
gui_group=None,
)
cpacs_inout.add_input(
var_name='delete_old_wkdirs',
var_type=bool,
default_value=False,
unit=None,
descr="Delete old PyTornado working directories (if existent)",
xpath=XPATH_PYTORNADO + '/deleteOldWKDIRs',
gui=False,
gui_name='Delete',
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
include_gui = True
# ----- Input -----
cpacs_inout.add_input(
var_name='Objectives',
var_type=str,
default_value='cl',
unit='-',
descr="""Objective function list for the surrogate model to predict \n Warning !
The parameters name must match the ones in the CSV file !""",
xpath=CEASIOM_XPATH+'/surrogateModel/objective',
gui=include_gui,
gui_name='Objective',
gui_group='Global settings',
)
cpacs_inout.add_input(
var_name='trainig_part',
var_type=float,
default_value='0.9',
descr='Defining the percentage of the data to use to train the model in [0;1]',
xpath=CEASIOM_XPATH+'/surrogateModel/trainingPercentage',
gui=include_gui,
gui_name='% of training data',
gui_group='Global settings'
# ===== Results directory path =====
RESULTS_DIR = Path("Results", "SUMO")
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ----- Input -----
cpacs_inout.add_input(
var_name="sumo_file_path",
var_type="pathtype",
default_value="-",
unit="1",
descr="Absolute path to the SUMO file",
xpath=SUMOFILE_XPATH,
gui=True,
gui_name="SUMO File path",
gui_group="Inputs",
)
cpacs_inout.add_input(
var_name="refine_level",
var_type="float",
default_value=1.0,
unit="1",
descr="0 is baseline, +1 env. equal double mesh points",
xpath=MESH_XPATH + "/sumoOptions/refinementLevel",
gui=True,
gui_name="Refinement Level",
#!/usr/bin/env python3
# -*- coding: utf-8 -*-
from ceasiompy.utils.moduleinterfaces import CPACSInOut, CEASIOM_XPATH, AIRCRAFT_XPATH
cpacs_inout = CPACSInOut()
# ===== Input =====
cpacs_inout.add_input(
var_name='mtom',
default_value=None,
unit='kg',
descr='MTOM (maybe another mass shoud be used, more representative for cruise mass?)',
cpacs_path=AIRCRAFT_XPATH + '/model/analyses/massBreakdown/designMasses/mTOM/mass',
)
cpacs_inout.add_input(
var_name='cruise_mach',
default_value=0.78,
unit='-',
descr='Aircraft cruise Mach number',
cpacs_path=CEASIOM_XPATH + '/ranges/cruiseMach',
)
cpacs_inout.add_input(
var_name='cruise_alt',
default_value=12000,
unit='m',
descr='Aircraft cruise altitude',
cpacs_path=CEASIOM_XPATH + '/ranges/cruiseAltitude',
"author": "Vivien Riolo",
"email": "*****@*****.**",
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
include_gui = True
# ----- Input -----
cpacs_inout.add_input(var_name='model_file',
var_type='pathtype',
default_value='-',
descr='File that contains a trained model',
xpath=CEASIOM_XPATH + '/surrogateModelUse/modelFile',
gui=include_gui,
gui_name='Model to use',
gui_group='Prediction options')
cpacs_inout.add_input(
var_name='Aeromap only',
var_type=bool,
default_value='False',
unit=None,
descr=
"""Indicate wether or not the parameters are all contained in an aeromap, in which case
the workflow only has to be run once.""",
xpath=CEASIOM_XPATH + '/surrogateModelUse/AeroMapOnly',
gui=include_gui,
gui_name='Aeromap only',
# -*- coding: utf-8 -*-
from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import PLOT_XPATH
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ===== Input =====
cpacs_inout.add_input(
var_name="",
var_type=list,
default_value=None,
descr="List of aeroMap to plot",
xpath=PLOT_XPATH + "/aeroMapToPlot",
gui=True,
gui_name="__AEROMAP_CHECHBOX",
# gui_group='Multipe aeromap'
)
cpacs_inout.add_input(
var_name="alt_crit",
var_type=str,
default_value="None",
descr="Altitude inclusion criteria",
xpath=PLOT_XPATH + "/criterion/alt",
gui=True,
gui_name="Altitdue criteria",
gui_group="Plot vs AoA",
)
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
include_gui = True
# ----- Input -----
cpacs_inout.add_input(
var_name='Objective function',
var_type=str,
default_value='cl/cd',
unit='-',
descr="""Objective function of the optimisation problem. \n Warning !
The parameters name must match the ones in the CSV file !""",
xpath=CEASIOM_XPATH + '/Optimisation/objective',
gui=include_gui,
gui_name='Objective',
gui_group='Objective function',
)
cpacs_inout.add_input(var_name='minmax',
var_type=list,
default_value=['min', 'max'],
unit='-',
descr='Objective function of the optimisation problem',
xpath=CEASIOM_XPATH + '/Optimisation/minmax',
gui=include_gui,
gui_name='Optimisation goal',
gui_group='Global settings')
#!/usr/bin/env python3
# -*- coding: utf-8 -*-
from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import GEOM_XPATH, RANGE_XPATH, SF_XPATH, PLOT_XPATH
cpacs_inout = CPACSInOut()
# ===== Input =====
cpacs_inout.add_input(
var_name="",
var_type=list,
default_value=None,
descr="To which aeroMap the skin friction coef should be added",
xpath=SF_XPATH + "/aeroMapToCalculate",
gui=True,
gui_name="__AEROMAP_CHECHBOX",
)
cpacs_inout.add_input(
var_name="wetted_area",
var_type=float,
default_value=None,
unit="m^2",
descr="Wetted area of the aircraft (calculated by SU2)",
xpath=GEOM_XPATH + "/analysis/wettedArea",
gui=False,
gui_name="Wetted Area",
gui_group=None,
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ===== Input =====
cpacs_inout.add_input(
var_name='',
var_type=list,
default_value=None,
unit=None,
descr="Name of the aero map to evaluate",
xpath=STABILITY_DYNAMIC_XPATH + '/aeroMapUid',
gui=True,
gui_name='__AEROMAP_SELECTION',
gui_group='Inputs',
)
cpacs_inout.add_input(
var_name='MassConfig',
var_type=list,
default_value= ['mMLM', 'mMRM', 'mTOM', 'mZFM'],
unit='[unit]',
xpath='/cpacs/toolspecific/CEASIOMpy/stability/dynamic/MassConfiguration',
gui=True,
gui_name='Mass selection: ',
gui_group='Inputs'
"author": "Aidan Jungo",
"email": "*****@*****.**",
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ----- Input -----
cpacs_inout.add_input(
var_name='aeromap_uid',
var_type=list,
default_value=None,
unit=None,
descr="Name of the aero map to calculate",
xpath=CEASIOM_XPATH + '/aerodynamics/su2/aeroMapUID',
gui=True,
gui_name='__AEROMAP_SELECTION',
gui_group=None,
)
cpacs_inout.add_input(
var_name='ref_len',
var_type=float,
default_value=None,
unit='m',
descr='Reference length of the aircraft',
xpath=AIRCRAFT_XPATH + '/model/reference/length',
gui=False,
gui_name=None,
"author": "Aidan Jungo",
"email": "*****@*****.**",
}
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ----- Input -----
cpacs_inout.add_input(
var_name='sumo_file_path',
var_type='pathtype',
default_value='-',
unit='1',
descr='Absolute path to the SUMO file',
xpath=CEASIOM_XPATH + '/filesPath/sumoFilePath',
gui=True,
gui_name='SUMO File path',
gui_group='Inputs',
)
cpacs_inout.add_input(
var_name='refine_level',
var_type='float',
default_value=0.0,
unit='1',
descr='0 is baseline, +1 env. equal double mesh points',
xpath=CEASIOM_XPATH + '/mesh/sumoOptions/refinementLevel',
gui=True,
gui_name='Refinement Level',
RESULTS_DIR = Path("Results", "SUMO")
# ===== CPACS inputs and outputs =====
cpacs_inout = CPACSInOut()
# ----- Input -----
cpacs_inout.add_input(
var_name="include_engine",
var_type=bool,
default_value=False,
unit="1",
descr="Convert engine from CEASIOMpy",
xpath=CEASIOMPY_XPATH + "/engine/includeEngine",
gui=True,
gui_name="Include engine",
gui_group="Option",
)
cpacs_inout.add_input(
var_name="include_pylon",
var_type=bool,
default_value=False,
unit="1",
descr="Convert engine from CEASIOMpy",
xpath=CEASIOMPY_XPATH + "/engine/includePylon",
gui=True,
gui_name="Include pylon",
