SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero Class Reference
Inheritance diagram for SUAVE.Analyses.Noise.Fidelity_Zero.Fidelity_Zero:
SUAVE.Analyses.Noise.Noise.Noise SUAVE.Analyses.Analysis.Analysis

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
 

Detailed Description

SUAVE.Analyses.Noise.Fidelity_Zero()

    The Fidelity Zero Noise Analysis Class
    
        Assumptions:
        None
        
        Source:
        N/A

Member Function Documentation

◆ __defaults__()

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.

◆ evaluate_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

◆ finalize()

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.


The documentation for this class was generated from the following file: