Public Member Functions | |
def | __defaults__ (self) |
def | finalize (self) |
def | __call__ (self, conditions) |
Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability | |
def | evaluate (self, conditions) |
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 | |
configuration | |
geometry | |
Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability | |
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.Stability.Fidelity_Zero.Fidelity_Zero.__call__ | ( | self, | |
conditions | |||
) |
Process vehicle to setup geometry, condititon and configuration Assumptions: None Source: N/4 Inputs: conditions - DataDict() of aerodynamic conditions results - DataDict() of moment coeffients and stability and body axis derivatives Outputs: None Properties Used: self.geometry
def SUAVE.Analyses.Stability.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.Stability.Stability.Stability.
def SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.finalize | ( | self | ) |
Finalizes the surrogate needed for lift calculation. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: self.geometry
Reimplemented from SUAVE.Analyses.Stability.Stability.Stability.