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

Public Member Functions

def __defaults__ (self)
- 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


Detailed Description

This class defines the control surface geometry and deflection

Member Function Documentation

◆ __defaults__()

def SUAVE.Methods.Aerodynamics.AVL.Data.Wing.Control_Surface_Results.__defaults__ (   self)
Sets the defaults of the control surface on the aircraft wing

Reimplemented from SUAVE.Core.Data.Data.

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