Public Member Functions | |
| def | __defaults__ (self) |
| def | finalize (self) |
| def | evaluate_noise (self, conditions) |
Public Member Functions inherited from SUAVE.Analyses.Noise.Noise.Noise | |
| def | evaluate (self, state) |
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 | |
| geometry | |
| flyover | |
| approach | |
| sideline | |
Public Attributes inherited from SUAVE.Analyses.Noise.Noise.Noise | |
| tag | |
| geometry | |
| settings | |
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis | |
| tag | |
| features | |
| settings | |
SUAVE.Analyses.Noise.Fidelity_Zero()
The Fidelity Zero Noise Analysis Class
Assumptions:
None
Source:
N/A
| def SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.__defaults__ | ( | self | ) |
This sets the default values for the analysis. Assumptions: None Source: N/A Inputs: None Output: None Properties Used: N/A
Reimplemented from SUAVE.Analyses.Noise.Noise.Noise.
| def SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero.evaluate_noise | ( | 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.Noise.Fidelity_Zero.Fidelity_Zero.finalize | ( | self | ) |
Finalizes the surrogate needed for lift calculation.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
None
Reimplemented from SUAVE.Analyses.Noise.Noise.Noise.