Public Member Functions | |
| def | __defaults__ (self) |
Public Member Functions inherited from SUAVE.Components.Wings.Wing.Wing | |
| def | append_segment (self, segment) |
| def | append_airfoil (self, airfoil) |
| def | append_control_surface (self, control_surface) |
| def | append_fuel_tank (self, fuel_tank) |
Public Attributes | |
| tag | |
| sign_duplicate | |
Public Attributes inherited from SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail | |
| tag | |
| generative_design_max_per_vehicle | |
Public Attributes inherited from SUAVE.Components.Wings.Wing.Wing | |
| tag | |
| mass_properties | |
| origin | |
| symmetric | |
| vertical | |
| t_tail | |
| taper | |
| dihedral | |
| aspect_ratio | |
| thickness_to_chord | |
| aerodynamic_center | |
| exposed_root_chord_offset | |
| total_length | |
| spans | |
| areas | |
| chords | |
| sweeps | |
| twists | |
| high_lift | |
| symbolic | |
| high_mach | |
| vortex_lift | |
| transition_x_upper | |
| transition_x_lower | |
| dynamic_pressure_ratio | |
| Airfoil | |
| non_dimensional_origin | |
| generative_design_minimum | |
| generative_design_max_per_vehicle | |
| generative_design_characteristics | |
| generative_design_char_min_bounds | |
| generative_design_char_max_bounds | |
| Segments | |
| control_surfaces | |
| Fuel_Tanks | |
Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body | |
| tag | |
| Segments | |
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 | |
Public Attributes inherited from SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface | |
| tag | |
| sign_duplicate | |
| hinge_fraction | |
| deflection | |
| use_constant_hinge_fraction | |
| hinge_vector | |
This class is used to define stabilators in SUAVE. Note that it
inherits from both Horizontal_Tail and All_Moving_Surface
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A | def SUAVE.Components.Wings.Stabilator.Stabilator.__defaults__ | ( | self | ) |
This sets the default for stabilators in SUAVE.
See All_Moving_Surface().__defaults__ and Wing().__defaults__ for
an explanation of attributes
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
Reimplemented from SUAVE.Components.Wings.All_Moving_Surface.All_Moving_Surface.