SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator Class Reference
Inheritance diagram for SUAVE.Components.Wings.Control_Surfaces.Elevator.Elevator:
SUAVE.Components.Wings.Control_Surfaces.Control_Surface.Control_Surface SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component

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.Elevator.Elevator.__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.


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