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SUAVE
2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
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SUAVE
2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
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Public Member Functions | |
| def | __defaults__ (self) |
| 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 | |
| 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 | |
This class defines the wing in SUAVE Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
| def SUAVE.Components.Wings.Wing.Wing.__defaults__ | ( | self | ) |
This sets the default values of a wing defined in SUAVE.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
Reimplemented from SUAVE.Components.Lofted_Body.Lofted_Body.
Reimplemented in SUAVE.Components.Wings.Main_Wing.Main_Wing, SUAVE.Components.Wings.Vertical_Tail.Vertical_Tail, SUAVE.Components.Wings.Stabilator.Stabilator, SUAVE.Components.Wings.Vertical_Tail_All_Moving.Vertical_Tail_All_Moving, and SUAVE.Components.Wings.Horizontal_Tail.Horizontal_Tail.
| def SUAVE.Components.Wings.Wing.Wing.append_airfoil | ( | self, | |
| airfoil | |||
| ) |
Adds an airfoil to the segment
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
| def SUAVE.Components.Wings.Wing.Wing.append_control_surface | ( | self, | |
| control_surface | |||
| ) |
Adds a component to vehicle
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
| def SUAVE.Components.Wings.Wing.Wing.append_fuel_tank | ( | self, | |
| fuel_tank | |||
| ) |
Adds a fuel tank to the wing
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
| def SUAVE.Components.Wings.Wing.Wing.append_segment | ( | self, | |
| segment | |||
| ) |
Adds a segment to the wing
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
1.8.15