SUAVE.Components.Airfoils.Airfoil.Airfoil Class Reference

Inheritance diagram for SUAVE.Components.Airfoils.Airfoil.Airfoil:

Public Member Functions
def	__defaults__ (self)

Public Attributes
	tag
	thickness_to_chord
	naca_4_series_airfoil
	coordinate_file
	points
Public Attributes inherited from SUAVE.Components.Lofted_Body.Section
	tag
	prev
	next
Public Attributes inherited from SUAVE.Components.Component.Component
	tag
	origin
	generative_design_max_per_vehicle
	generative_design_characteristics
	generative_design_special_parent

Member Function Documentation

__defaults__()

def SUAVE.Components.Airfoils.Airfoil.Airfoil.__defaults__

(

self

)

This sets the default values of a airfoil defined in SUAVE.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Components.Lofted_Body.Section.

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The documentation for this class was generated from the following file:

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Airfoils/Airfoil.py