Description. More...
Functions | |
def | SUAVE.Plots.Geometry.plot_propeller.plot_propeller (prop, face_color='red', edge_color='black', save_figure=False, save_filename="Propeller_Geometry", file_type=".png") |
def | SUAVE.Plots.Geometry.plot_vehicle.plot_vehicle (vehicle, elevation_angle=30, azimuthal_angle=210, axis_limits=10, plot_axis=False, save_figure=False, plot_control_points=True, save_filename="Vehicle_Geometry") |
def | SUAVE.Plots.Geometry.plot_vehicle_vlm_panelization.plot_vehicle_vlm_panelization (vehicle, elevation_angle=30, azimuthal_angle=210, axis_limits=10, plot_axis=False, save_figure=False, plot_control_points=True, save_filename="VLM_Panelization") |
Description.
def SUAVE.Plots.Geometry.plot_propeller.plot_propeller | ( | prop, | |
face_color = 'red' , |
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edge_color = 'black' , |
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save_figure = False , |
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save_filename = "Propeller_Geometry" , |
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file_type = ".png" |
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) |
This plots the geometry of a propeller or rotor Assumptions: None Source: None Inputs: SUAVE.Components.Energy.Converters.Propeller() Outputs: Plots Properties Used: N/A
def SUAVE.Plots.Geometry.plot_vehicle.plot_vehicle | ( | vehicle, | |
elevation_angle = 30 , |
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azimuthal_angle = 210 , |
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axis_limits = 10 , |
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plot_axis = False , |
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save_figure = False , |
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plot_control_points = True , |
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save_filename = "Vehicle_Geometry" |
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) |
This plots vortex lattice panels created when Fidelity Zero Aerodynamics Routine is initialized Assumptions: None Source: None Inputs: vehicle Outputs: Plots Properties Used: N/A
def SUAVE.Plots.Geometry.plot_vehicle_vlm_panelization.plot_vehicle_vlm_panelization | ( | vehicle, | |
elevation_angle = 30 , |
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azimuthal_angle = 210 , |
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axis_limits = 10 , |
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plot_axis = False , |
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save_figure = False , |
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plot_control_points = True , |
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save_filename = "VLM_Panelization" |
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) |
This plots vortex lattice panels created when Fidelity Zero Aerodynamics Routine is initialized Assumptions: None Source: None Inputs: vehicle.vortex_distribution Outputs: Plots Properties Used: N/A