#  This file is part of FAST-OAD_CS23 : A framework for rapid Overall Aircraft Design
#  Copyright (C) 2025  ONERA & ISAE-SUPAERO
#  FAST is free software: you can redistribute it and/or modify
#  it under the terms of the GNU General Public License as published by
#  the Free Software Foundation, either version 3 of the License, or
#  (at your option) any later version.
#  This program is distributed in the hope that it will be useful,
#  but WITHOUT ANY WARRANTY; without even the implied warranty of
#  MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
#  GNU General Public License for more details.
#  You should have received a copy of the GNU General Public License
#  along with this program.  If not, see <https://www.gnu.org/licenses/>.


from .analysis_and_plots import (
    aircraft_geometry_plot,
    evolution_diagram,
    compressibility_effects_diagram,
    cl_wing_diagram,
    drag_breakdown_diagram,
    aircraft_polar,
    cg_lateral_diagram,
    mass_breakdown_bar_plot,
    mass_breakdown_sun_plot,
    payload_range,
)
from .load_analysis.analysis_and_plots_la import (
    force_repartition_diagram,
    rbm_diagram,
    shear_diagram,
)
from .propeller.analysis_and_plots_propeller import (
    propeller_efficiency_map_plot,
    propeller_coeff_map_plot,
)

__all__ = [
    "aircraft_geometry_plot",
    "evolution_diagram",
    "compressibility_effects_diagram",
    "cl_wing_diagram",
    "drag_breakdown_diagram",
    "aircraft_polar",
    "cg_lateral_diagram",
    "mass_breakdown_bar_plot",
    "mass_breakdown_sun_plot",
    "payload_range",
    "force_repartition_diagram",
    "rbm_diagram",
    "shear_diagram",
    "propeller_efficiency_map_plot",
    "propeller_coeff_map_plot",
]
