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.