SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing Class Reference
Inheritance diagram for SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing:
SUAVE.Core.Data.Data

Public Member Functions

def __defaults__ (self)
 
def append_section (self, section)
 
- Public Member Functions inherited from SUAVE.Core.Data.Data
def __getattribute__ (self, k)
 
def __setattr__ (self, k, v)
 
def __delattr__ (self, k)
 
def __new__ (cls, *args, **kwarg)
 
def typestring (self)
 
def dataname (self)
 
def __str__ (self, indent='')
 
def __init__ (self, *args, **kwarg)
 
def __iter__ (self)
 
def itervalues (self)
 
def values (self)
 
def update (self, other)
 
def append_or_update (self, other)
 
def get_bases (self)
 
def append (self, value, key=None)
 
def deep_set (self, keys, val)
 
def deep_get (self, keys)
 
def pack_array (self, output='vector')
 
def unpack_array (self, M)
 
def do_recursive (self, method, other=None, default=None)
 

Public Attributes

 tag
 
 symmetric
 
 vertical
 
 origin
 
 sweep
 
 dihedral
 
 sections
 
 configuration
 
 control_surfaces
 

Detailed Description

This class that defines parameters of the AVL aircraft wing

Assumptions:
    None

Source:
    None

Inputs:
    None

Outputs:
    None

Properties Used:
    N/A

Member Function Documentation

◆ __defaults__()

def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing.__defaults__ (   self)
A stub for all classes that come later
    
    Assumptions:
    N/A
    
    Source:
    N/A
    
    Inputs:
    N/A
    
    Outputs:
    N/A
    
    Properties Used:
    N/A    

Reimplemented from SUAVE.Core.Data.Data.

◆ append_section()

def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Wing.append_section (   self,
  section 
)
Adds a segment to the wing 

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