SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail Class Reference

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

Public Member Functions
def	__defaults__ (self)
Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing
def	append_segment (self, segment)
def	append_airfoil (self, airfoil)
def	append_control_surface (self, control_surface)
def	append_fuel_tank (self, fuel_tank)

Public Attributes
	tag
	generative_design_max_per_vehicle
Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing
	tag
	mass_properties
	origin
	symmetric
	vertical
	t_tail
	taper
	dihedral
	aspect_ratio
	thickness_to_chord
	aerodynamic_center
	exposed_root_chord_offset
	total_length
	spans
	areas
	chords
	sweeps
	twists
	high_lift
	symbolic
	high_mach
	vortex_lift
	transition_x_upper
	transition_x_lower
	dynamic_pressure_ratio
	Airfoil
	non_dimensional_origin
	generative_design_minimum
	generative_design_max_per_vehicle
	generative_design_characteristics
	generative_design_char_min_bounds
	generative_design_char_max_bounds
	Segments
	control_surfaces
	Fuel_Tanks
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 class is used to define horiontal tails SUAVE

    Assumptions:
    None

    Source:
    N/A

    Inputs:
    None

    Outputs:
    None

    Properties Used:
    N/A

Member Function Documentation

__defaults__()

def SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail.__defaults__

(

self

)

This sets the default for horizontal tails in SUAVE.
    
Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Components.Wings.Wing.Wing.

Reimplemented in SUAVE.Components.Wings.Stabilator.Stabilator.

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

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