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:
SUAVE.Core.Data.Data

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

 tag
 
 deflection
 
 CL
 
 CY
 
 Cl
 
 Cm
 
 Cn
 
 CDff
 
 e
 

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: