from MARILib.aircraft_model.operations import handling_qualities as h_q,\
mission as perfo, \
environmental_impact as environ, \
pricing_and_costing as costing
from MARILib.aircraft_model.airplane import regulation as regul, \
airplane_design as airplane, \
aerodynamics as craft_aero, viewer as show
from MARILib.aircraft_model import initialization as init
from MARILib.processes import solvers as sub_proc
# Initialize aircraft data structure
#------------------------------------------------------------------------------------------------------
ac = Aircraft()
design_range = unit.m_NM(3000)
cruise_mach = 0.78
n_pax_ref = 150
propulsive_architecture = init.prop_architecture()
ac.propulsion.architecture = propulsive_architecture
ac.propulsion.fuel_type = init.fuel_type()
n_engine = init.n_engine()
ac.name = "my_test_airplane"
ac.design_driver.design_range = design_range # TLR
ac.design_driver.cruise_mach = cruise_mach # TLR
This study allows to illustrate the integration of a partial turbo-electric airplane
"""
from MARILib.tools import units as unit
from MARILib.earth import environment as earth
from MARILib.airplane.propulsion import propulsion_models as propu
from MARILib.aircraft_data.aircraft_description import Aircraft
from MARILib.processes import design as run
from MARILib.aircraft_model.airplane import viewer as show
# Initialize aircraft data structure
#------------------------------------------------------------------------------------------------------
aircraft = Aircraft()
design_range = unit.m_NM(3000)
cruise_mach = 0.78
n_pax_ref = 150
propulsion_architecture = 3
n_engine = 2
# Initialize all input data
#------------------------------------------------------------------------------------------------------
run.aircraft_initialize(aircraft, n_pax_ref, design_range, cruise_mach,
propulsion_architecture, n_engine)
# Possibility to modify initial values
#------------------------------------------------------------------------------------------------------
"""
from MARILib.tools import units as unit
from MARILib.aircraft_model.airplane import viewer as show
from MARILib.aircraft_model import initialization as init
from MARILib.aircraft_data.aircraft_description import Aircraft
from MARILib.processes import design as perform
# Initialize aircraft data structure
#------------------------------------------------------------------------------------------------------
architecture = init.prop_architecture()
aircraft = Aircraft(architecture)
design_range = 14800000 #unit.m_NM(8000)
cruise_mach = 0.85
n_pax_ref = 240
propu_config = 1
n_engine = 4
#------------------------------------------------------------------------------------------------------
perform.aircraft_initialize(aircraft, n_pax_ref, design_range, cruise_mach,
propu_config, n_engine)
aircraft.wing.attachment = 1
print("-------------------------------------------")