SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail Class Reference
Inheritance diagram for SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail:
SUAVE.Components.Wings.Wing.Wing SUAVE.Components.Lofted_Body.Lofted_Body SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component SUAVE.Components.Wings.Stabilator.Stabilator

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.


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