Public Member Functions | |
def | __defaults__ (self) |
def | evaluate (self, state) |
def | initialize (self) |
Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics | |
def | finalize (self) |
Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis | |
def | compile (self, *args, **kwarg) |
def | initialize (self, *args, **kwarg) |
def | evaluate (self, *args, **kwarg) |
def | finalize (self, *args, **kwarg) |
def | __call__ (self, *args, **kwarg) |
Public Attributes | |
tag | |
geometry | |
process | |
Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics | |
tag | |
geometry | |
settings | |
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis | |
tag | |
features | |
settings | |
This is an intermediate class for aerodynamic analyses. Assumptions: None Source: N/A
def SUAVE.Analyses.Aerodynamics.Markup.Markup.__defaults__ | ( | self | ) |
This sets the default values and methods for the analysis. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
Reimplemented from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.
Reimplemented in SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag, SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, SUAVE.Analyses.Aerodynamics.AVL.AVL, and SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS.
def SUAVE.Analyses.Aerodynamics.Markup.Markup.evaluate | ( | self, | |
state | |||
) |
The default evaluate function. Assumptions: None Source: N/A Inputs: None Outputs: results <SUAVE data class> Properties Used: self.settings self.geometry
Reimplemented from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.
def SUAVE.Analyses.Aerodynamics.Markup.Markup.initialize | ( | self | ) |
The default finalize function. Calls the initialize process. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
Reimplemented in SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Aerodynamics.AVL.AVL, SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, and SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag.