Public Member Functions | |
| def | __defaults__ (self) |
| def | append_wing (self, wing) |
| def | append_body (self, body) |
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 | |
| wings | |
| bodies | |
A data class defining the entire AVL aircraft geometry
Assumptions:
None
Source:
None
Inputs:
None
Outputs:
None
Properties Used:
N/A
| def SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft.__defaults__ | ( | self | ) |
Defines the data structure and defaults of aircraft classes
Assumptions:
None
Source:
None
Inputs:
None
Outputs:
None
Properties Used:
N/A
Reimplemented from SUAVE.Core.Data.Data.
| def SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft.append_body | ( | self, | |
| body | |||
| ) |
Appends body geometry onto aircraft class
Assumptions:
None
Source:
None
Inputs:
None
Outputs:
None
Properties Used:
N/A
| def SUAVE.Methods.Aerodynamics.AVL.Data.Aircraft.Aircraft.append_wing | ( | self, | |
| wing | |||
| ) |
Appends wing geometry onto aircraft class
Assumptions:
None
Source:
None
Inputs:
None
Outputs:
None
Properties Used:
N/A