Public Member Functions | |
def | __defaults__ (self) |
def | initialize (self) |
Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup | |
def | evaluate (self, state) |
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 | |
Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup | |
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 analysis based on low-fidelity models. Assumptions: Subsonic Source: Primarily based on adg.stanford.edu, see methods for details
def SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero.__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.Markup.Markup.
def SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero.initialize | ( | self | ) |
Initializes the surrogate needed for lift calculation. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: self.geometry
Reimplemented from SUAVE.Analyses.Aerodynamics.Markup.Markup.