SUAVE.Components.Fuselages.Fuselage.Fuselage Class Reference

Inheritance diagram for SUAVE.Components.Fuselages.Fuselage.Fuselage:

Public Member Functions
def	__defaults__ (self)
def	append_segment (self, segment)
def	append_fuel_tank (self, fuel_tank)

Public Attributes
	tag
	origin
	aerodynamic_center
	max_per_vehicle
	number_coach_seats
	seats_abreast
	seat_pitch
	areas
	effective_diameter
	width
	nose_curvature
	tail_curvature
	heights
	x_rotation
	y_rotation
	z_rotation
	lengths
	fineness
	differential_pressure
	aft_centerbody_area
	aft_centerbody_taper
	cabin_area
	non_dimensional_origin
	generative_design_minimum
	generative_design_max_per_vehicle
	generative_design_characteristics
	generative_design_char_min_bounds
	generative_design_char_max_bounds
	Fuel_Tanks
	vsp_data
	Segments
Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
	tag
	Segments
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 is a standard fuselage for a tube and wing aircraft.

Assumptions:
Conventional fuselage

Source:
N/A

Member Function Documentation

__defaults__()

def SUAVE.Components.Fuselages.Fuselage.Fuselage.__defaults__

(

self

)

This sets the default values for the component to function.

Assumptions:
None
    
Source:
N/A
    
Inputs:
None
    
Outputs:
None
    
Properties Used:
None

Reimplemented from SUAVE.Components.Lofted_Body.Lofted_Body.

append_fuel_tank()

def SUAVE.Components.Fuselages.Fuselage.Fuselage.append_fuel_tank	(		self,
			fuel_tank
	)

Adds a fuel tank to the fuselage 
    
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A

append_segment()

def SUAVE.Components.Fuselages.Fuselage.Fuselage.append_segment	(		self,
			segment
	)

Adds a segment to the fuselage. 
    
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/Fuselages/Fuselage.py