SUAVE.Components.Wings.Segment.Segment Class Reference

Inheritance diagram for SUAVE.Components.Wings.Segment.Segment:

Public Member Functions
def	__defaults__ (self)
def	append_airfoil (self, airfoil)

Public Attributes
	tag
	percent_span_location
	twist
	taper
	root_chord_percent
	dihedral_outboard
	thickness_to_chord
	sweeps
	chords
	areas
	Airfoil
	generative_design_minimum
	generative_design_max_per_vehicle
	generative_design_special_parent
	generative_design_characteristics
	generative_design_char_min_bounds
	generative_design_char_max_bounds
Public Attributes inherited from SUAVE.Components.Lofted_Body.Segment
	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.Wings.Segment.Segment.__defaults__

(

self

)

This sets the default for wing segments in SUAVE.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Components.Lofted_Body.Segment.

append_airfoil()

def SUAVE.Components.Wings.Segment.Segment.append_airfoil	(		self,
			airfoil
	)

Adds an airfoil to the segment

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Segment.py