Plots

Plots contains functions for generating common figures. More...

Modules
	Geometry
	Description.
	Performance
	Plots contains functions for generating common figures.

Functions
def	SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_boundary_layer_properties (ap, show_legend=True)
def	SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_polars (ap, show_legend=True)
def	SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_surface_forces (ap, show_legend=True, arrow_color='r')
def	SUAVE.Plots.Performance.Mission_Plots.plot_stability_coefficients (results, line_color='bo-', save_figure=False, save_filename="Stability_Coefficients", file_type=".png")

Detailed Description

Plots contains functions for generating common figures.

Function Documentation

plot_airfoil_analysis_boundary_layer_properties()

def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_boundary_layer_properties	(		ap,
			show_legend = True
	)

This plots the boundary layer properties of an airfoil
    or group of airfoils

    Assumptions:
    None
    
    Inputs: 
    ap       - data stucture of airfoil boundary layer properties  
    
    Outputs: 
    None 
    
    Properties Used:
    N/A

plot_airfoil_analysis_polars()

def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_polars	(		ap,
			show_legend = True
	)

This plots the polars of an airfoil or group of airfoils

    Assumptions:
    None
    
    Inputs: 
    ap       - data stucture of airfoil boundary layer properties and polars 
     
    Outputs: 
    None 
    
    Properties Used:
    N/A

plot_airfoil_analysis_surface_forces()

def SUAVE.Plots.Performance.Airfoil_Plots.plot_airfoil_analysis_surface_forces	(		ap,
			show_legend = True,
			arrow_color = 'r'
	)

This plots the forces on an airfoil surface

    Assumptions:
    None
    
    Inputs: 
    ap       - data stucture of airfoil boundary layer properties and polars 
     
    Outputs: 
    None 
    
    Properties Used:
    N/A

plot_stability_coefficients()

def SUAVE.Plots.Performance.Mission_Plots.plot_stability_coefficients	(		results,
			line_color = 'bo-',
			save_figure = False,
			save_filename = "Stability_Coefficients",
			file_type = ".png"
	)

This plots the static stability characteristics of an aircraft

Assumptions:
None

Source:
None

Inputs:
results.segments.conditions.stability.
   static
       CM 
       Cm_alpha 
       static_margin 
   aerodynamics.
       angle_of_attack
Outputs: 
Plots

Properties Used:
N/A