SUAVE.Components.Wings.Control_Surfaces.Flap.Flap Class Reference

Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Flap.Flap:

Public Member Functions
def	__defaults__ (self)

Public Attributes
	tag
	hinge_fraction
	sign_duplicate
Public Attributes inherited from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface
	tag
	span
	span_fraction_start
	span_fraction_end
	hinge_fraction
	chord_fraction
	sign_duplicate
	deflection
	configuration_type
	gain
Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
	tag
	mass_properties
	origin
	symmetric
Public Attributes inherited from SUAVE.Components.Component.Component
	tag
	origin
	generative_design_max_per_vehicle
	generative_design_characteristics
	generative_design_special_parent

Detailed Description

This class is used to define slats in SUAVE

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Member Function Documentation

__defaults__()

def SUAVE.Components.Wings.Control_Surfaces.Flap.Flap.__defaults__

(

self

)

This sets the default for slats in SUAVE.

see Control_Surface().__defaults__ for an explanation of attributes
    
Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface.

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Wings/Control_Surfaces/Flap.py